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Article

Space Development Capacity Building in Emerging Countries: A Technology Ladder Approach to Satellite Systems

by
Tetsuhito Fuse
1,2,*,
Eliza Sapkota
2,
Nobuaki Minato
1 and
Raihana Shams Islam Antara
2
1
Graduate School of Technology Management, Ritsumeikan University, 2-150 Iwakura-cho, Ibaraki 567-8570, Osaka, Japan
2
Laboratory of Lean Satellite Enterprises and In-Orbit Experiments (LaSEINE) Kyushu Institute of Technology, 1-1 Sensui Tobata-ku, Kitakyushu 804-8550, Fukuoka, Japan
*
Author to whom correspondence should be addressed.
Aerospace 2026, 13(4), 330; https://doi.org/10.3390/aerospace13040330
Submission received: 1 March 2026 / Revised: 25 March 2026 / Accepted: 29 March 2026 / Published: 1 April 2026
(This article belongs to the Section Astronautics & Space Science)

Abstract

The growing accessibility of small satellite technologies and international cooperation frameworks has enabled many emerging countries to initiate space development activities; however, the mechanisms through which they build and advance satellite development capabilities remain insufficiently theorized, as existing models such as the Space Technology Ladder capture only high-level milestones. To address this gap, this study proposes the Satellite Technology Ladder (SaTL), a structured 16-level framework integrating satellite development methods and satellite size as indicators of technological maturity. We conducted a comprehensive longitudinal analysis of all satellite projects initiated since 1990 across 16 emerging countries, coding each project according to the SaTL scheme and evaluating national trajectories over time. The analysis reveals four distinct developmental trajectories: (1) prolonged dependence on foreign procurement, (2) gradual capability enhancement through externally supported development, (3) expansion of domestic industrial ecosystems following initial collaboration, and (4) independent development from the outset based on pre-existing technological foundations. These findings demonstrate that technological advancement depends not only on technology introduction but also on absorptive capacity, institutional learning, and broader industrial structures. SaTL thus offers a theoretically grounded and empirically validated tool for assessing capability formation and informing policy strategies in emerging spacefaring nations.

1. Introduction

1.1. Background

Over the past two decades, global space activities have undergone a profound transformation. Satellite miniaturization, the widespread adoption of standardized platforms such as CubeSats, and the growing availability of international cooperation programs have dramatically lowered the barriers to entry for space development [1]. It is observed that the rise of low-cost, accessible platforms like CubeSats has fundamentally altered the initial rungs of the Technology Ladder, providing a new entry point for nations to begin their journey toward indigenous space capabilities. The increasing number of countries launching their first satellites via CubeSats since 2010 serves as compelling evidence of this new paradigm. With the introduction of space technology, an increasing number of countries are acquiring satellite capabilities through CubeSats as the simplest style of development. Between 2007 and 2024, 42 countries successfully developed satellites using CubeSats. As a result, a steadily increasing number of emerging countries have initiated satellite programs for purposes including Earth observation, communication, disaster management, and capacity building. Historical analyses of first-satellite programs indicate that many of these countries begin by relying on foreign technological support before gradually shifting toward more autonomous development [2]. Alongside national initiatives, regional institutions—such as the African Space Agency, the Arab Space Coordination Group, and the Latin American and Caribbean Space Agency—have begun playing an increasingly significant role in facilitating knowledge sharing and collective capability formation [3].
Despite these developments, the mechanisms through which emerging countries acquire, internalize, and advance satellite development capabilities remain insufficiently theorized. Existing macro-level frameworks, particularly the Space Technology Ladder (STL), conceptualize national space capability progression through milestones such as LEO/GEO satellite ownership and independent launch capability [4]. While these models provide a useful high-level overview, they lack the granularity needed to capture the incremental learning processes that characterize contemporary satellite development. In the CubeSat era, countries frequently progress through intermediate stages—moving from procurement to externally supported development, and eventually toward domestic subsystem production and indigenous manufacturing. Yet comparative analyses of these processes remain limited, and there is no systematic framework that accounts for both development methods and technological complexity.
The broader literature on technology acquisition and innovation in emerging economies reinforces the importance of absorptive capacity, institutional learning, and industrial foundations as determinants of successful capability formation [5]. Studies in adjacent sectors, such as advanced manufacturing and construction engineering, demonstrate that technology transfer is rarely linear and often depends on organizational readiness, human resource development, and robust domestic networks [6]. In the space sector specifically, recent research emphasizes the heterogeneity of technology sources—including foreign procurement, international cooperation, domestic R&D programs, and foreign direct investment—and the complex ways these sources interact to shape national innovation trajectories [7]. However, existing work does not provide a comparative, cross-national framework capable of explaining why some emerging countries advance rapidly while others remain technologically stagnant.
Against this backdrop, the present study introduces the Satellite Technology Ladder (SaTL), a new analytical framework designed to capture the finer-grained stages of satellite development capability. SaTL differs from STL by focusing exclusively on satellite manufacturing competencies and by integrating two analytically significant dimensions: (1) satellite development methods, which represent increasing levels of technological autonomy; and (2) satellite size categories, which proxy engineering complexity. By combining these dimensions into a 16-level taxonomy, SaTL offers a more precise tool for evaluating technological maturity and for analyzing developmental trajectories over time.
Using comprehensive data on all satellite projects initiated since 1990 across 16 emerging countries, this study reconstructs longitudinal development trajectories and identifies common patterns in capability formation. The contributions of this research are threefold. First, it refines the Technology Ladder concept to reflect the realities of modern satellite development. Second, it offers an empirical, cross-national analysis of how emerging countries progress technologically in the space sector. Third, it provides actionable insights for policymakers and space agencies regarding technology transfer strategies, capacity-building programs, and the development of sustainable space industry ecosystems.

1.2. Purpose

Against this historical background, this study examines how the research and development (R&D) system, once limited to government-led projects in a small number of developed countries—primarily the United States, the Soviet Union, Europe, and Japan—has evolved to include other players, such as developing countries, the private sector, and universities.
The purpose of this paper is to identify the technical level of the space development systems in emerging countries, with a particular focus on satellite development projects, and to analyze the progression of these systems. By defining the technological patterns of each country and examining their developmental trajectories, this study categorizes countries into those that have not established their own development systems and primarily rely on procurement from developed countries, those that have successfully transitioned to their own industries by effectively leveraging cooperation from developed nations, and those currently in the process of acquiring technologies, particularly in satellite development. This approach facilitates international comparisons of technology ladder classifications and aids in analyzing the transition process over time. By introducing SaTL and comparing countries, we will compare countries that have smoothly acquired technology through the introduction of space programs and have connected it to social implementation with countries that have remained at the initial stage of technology introduction and have not progressed further, and clarify what factors influence the acquisition and dissemination of technology.
Specifically, the study will investigate the development of satellite projects in various countries, focusing on the time frame and systems under which these projects were initiated, particularly in nations that embarked on space development relatively recently, after 1990. The research will comprehensively summarize the changes in development systems for each project. Finally, the study will propose a typology that illustrates the nature of these transitions with the discussion of Technology ladder theory and Stakeholder analysis. Although there are several definitions, in this paper, 1000 kg or less is referred to as Small Satellite, 100 kg or less is referred to as Nano Satellite, and 10 kg or less is referred to as CubeSat.

2. Literature Review

2.1. Satellite Development in Emerging Countries

The global expansion of small satellite technologies has reshaped the participation of emerging countries in the space sector. The proliferation of CubeSats, standardized bus architectures, and increasingly affordable launch opportunities has lowered entry barriers and enabled many nations to initiate satellite development for Earth observation, communications, and capacity-building purposes [1]. Early investigations show that developing countries typically launch their first satellites through foreign procurement or educational partnerships with established agencies, which serve both as training platforms and as mechanisms for institutional formation [2]. Over time, several nations—including Argentina, Turkiye, Malaysia, and South Africa—demonstrated gradual transitions from externally supported missions toward more autonomous development, facilitated by universities, aerospace SMEs, and publicly funded research institutions [8]. Parallel to these national initiatives, regional institutions such as the African Space Agency, the Arab Space Coordination Group, and the Latin American and Caribbean Space Agency have begun coordinating shared missions, pooling technical resources, and expanding human capital development programs. While these developments underscore a growing diversification of actors, most existing studies remain descriptive and do not provide systematic frameworks for assessing technological progression.

2.2. Technology Ladder and Capability Accumulation

The Technology Ladder has been widely employed to conceptualize how firms and nations accumulate increasingly sophisticated technological capabilities. Foundational work describes this process as an advancement from basic production toward adaptive engineering and ultimately system-level innovation [9,10]. Applied to the aerospace context, Wood’s Space Technology Ladder (STL) [4] represents an important attempt to classify national space capability milestones across satellite, launch, and operational domains. Although influential, STL faces several limitations when analyzed in light of contemporary satellite development. It aggregates multiple technological fields, thereby obscuring project-level engineering competence; it lacks the granularity needed to distinguish different levels of technological complexity among CubeSats, microsatellites, and larger satellites; and it assumes linear progression, despite empirical evidence showing hybrid and non-linear capability paths in emerging countries [8]. Studies in other sectors likewise demonstrate that latecomer innovation often follows branching trajectories shaped by institutional conditions, industrial specializations, and global value-chain integration [11]. These insights collectively suggest that a more flexible and granular model is needed to capture the dynamics of satellite capability-building.

2.3. Technology Acquisition, International Cooperation, and Learning Dynamics

The literature on technology acquisition in emerging economies offers additional perspective on satellite capability formation. According to absorptive capacity theory, organizations must possess sufficient prior knowledge and learning routines to effectively internalize external technology [5]. For complex engineering sectors such as aerospace, successful capability acquisition requires not only technology transfer but also complementary investments in training, system integration skills, and institutional coordination [10]. International technology transfer (ITT) programs, whether conducted through joint development, turnkey procurement, or university-led missions, play an essential role in accelerating early-stage learning. However, the sustainability of these gains depends on domestic institutional strength and long-term embedding of acquired knowledge in organizational practices [12].
Case studies from Nigeria’s NigComSat program [13], Turkiye’s dual-use satellite efforts [14], and Argentina’s CONAE–INVAP ecosystem illustrate the diversity of outcomes that emerge from different technology sourcing strategies [15]. Recent analyses argue that the interplay between external collaboration, domestic R&D, and industrial ecosystems strongly influence national innovation trajectories [7]. In adjacent sectors, university–industry collaboration has been shown to serve as a crucial engine for tacit knowledge formation and subsystem-level specialization [16]. Collectively, these studies underscore that satellite capability development is a cumulative, path-dependent process shaped by institutional complementarities, inter-organizational networks, and mission-oriented policy interventions.

2.4. Theory Integrates Engineering Complexity with Technology Acquisition Pathways

Although existing studies offer valuable insights into early satellite programs, national innovation systems, and international technology transfer, the literature remains fragmented and lacks a coherent analytical framework capable of capturing satellite-specific capability progression. Current models such as STL do not incorporate two key project-level dimensions central to understanding technological maturity, while this describes the progress of space development capability from the perspective of the national program. These limitations highlight the need for a satellite-focused capability model that integrates engineering complexity with technology acquisition pathways. By utilizing satellite projects—the definitive systems of aerospace technology—as a primary benchmark, this study enables a rigorous assessment of a nation’s space capabilities. This approach facilitates an evaluation of both technological maturity and the broader evolution of national space programs, providing a standardized metric for tracking sectoral development.
In response to this gap, the present study proposes the Satellite Technology Ladder (SaTL), a 16-level taxonomy that systematically classifies satellite development projects by combining development method and satellite size. This framework provides the analytical foundation necessary for conducting longitudinal, cross-national comparisons of capability formation. By grounding satellite capability research within broader theories of technological upgrading, national innovation systems, and latecomer development strategies, SaTL offers a more precise and theoretically consistent approach for evaluating how emerging countries build sustainable space-sector capabilities.

3. Research Method

This study adopts a qualitative–comparative research design to classify satellite development projects in emerging spacefaring nations and to examine their technological trajectories using the Satellite Technology Ladder (SaTL). Because the existing literature lacks standardized analytical instruments for comparing national satellite programs, the methodological approach emphasizes transparency, reproducibility, and cross-validation. The following subsections describe the procedures for data collection, operationalization of SaTL, coding reliability, analytical strategy, and bias mitigation.

3.1. Identification of Target Countries

First, the target countries for investigation are identified. Selected countries are those with relatively short histories of space development and economies that meet the definition of emerging countries. However, to accurately assess the development process of technology acquisition, we exclude countries that are still in the early stages, such as those that have launched only a single satellite. Specifically, countries meeting all three of the following criteria are selected as shown in the Table 1:
  • Classified as emerging countries according to UN standards [17] (World Economic Situation and Prospects 2024)
  • Initiated satellite development no earlier than 1990
  • Have a track record of developing more than five satellites by 2024
In the countries discussed in Section 3.2, we examined all emerging nations with satellite development achievements and identified the following 16 countries:

3.2. Data Collection and Sampling Strategy

A comprehensive dataset was constructed through systematic collection of satellite mission records launched or initiated between 1990 and 2024. The starting point of 1990 was chosen because it marked the period when small satellite technology became globally widespread, followed by the formalization of the CubeSat standard, significantly lowering barriers to entry for emerging space nations. It also captures over 30 years of project evolution. Data were obtained from official space agency repositories, university satellite program archives, international mission databases such as Gunter’s Space Page [18] and the Nanosats Database [19], peer-reviewed journal articles, conference proceedings, and government or industry reports. To ensure coverage across a broad range of national contexts, a country-by-country saturation strategy was applied, whereby data collection continued until no further verifiable missions or technical details could be identified. Eligibility required that each mission includes documented national involvement, publicly accessible development information, and classification under recognized satellite categories. Missions with insufficient documentation—especially early defense-related satellites—were excluded to avoid inferential bias.
A structured data extraction sheet standardized the collection of mission attributes, including satellite mass, subsystem configuration, development partners, technology procurement routes, training components, and the extent of domestic participation in design and manufacturing.

3.3. Operationalization of the Satellite Technology Ladder (SaTL)

SaTL is formulated as a 16-level classification system derived from the intersection of two analytically critical dimensions: development method and satellite size. To ensure construct validity, both dimensions were defined using explicit, replicable rules.

3.3.1. Development Method Classification

Development method was operationalized along a continuum of technological autonomy, ranging from full procurement to externally supported development, domestically supported development, and fully indigenous development. Coding for this dimension relied exclusively on documented engineering responsibilities rather than policy statements or media claims.
FP1 (Basic Foreign Procurement)
Entirely overseas development. No domestic involvement in design, manufacturing, or testing.
FP2 (Foreign Procurement with Training)
Overseas-led development, but domestic engineers gain formal learning opportunities such as observation, test participation, or short-term training. However, there is no domestic contribution to design or integration.
JD (Joint Development)
Domestic organizations substantially participate as co-developers in subsystem design, integration work, environmental testing, etc. Domestic technical contributions are essential for project execution.
DD (Domestic Development)
Domestic-led satellite design, integration, and testing. External companies play only a partial supporting role; major technical decisions are made domestically.
The following section delineates the boundaries for the four primary development methodologies: Foreign Partner 1 (FP1), Foreign Partner 2 (FP2), Joint Development (JD), and Domestic Development (DD). FP1 characterizes projects where the entire development process occurs within a foreign partner’s nation, typically with no recorded involvement from the emerging nation. Conversely, FP2 refers to projects where the foreign partner maintains primary responsibility, yet the emerging nation participates through activities such as operational training or capacity building. Crucially, if the emerging nation’s involvement is limited to procurement-related tasks—such as conducting final acceptance inspections—the project remains classified as FP1. A prominent example of FP2 is the Kyushu Institute of Technology’s (Kyutech) BIRDS program. While development for these projects occurred in Japan, 2 to 3 students from each of the 13 partner countries were embedded at Kyutech to pursue advanced degrees and contribute directly to the development process [20]. JD denotes projects led primarily by the emerging nation with external technical support. For instance, while Indonesia’s LAPAN-TUBSAT was classified as FP2 due to the dominant role of Berlin Space Technologies (BST), the subsequent LAPAN-A2 and A3 satellites shifted to JD [21]. Although BST provided several subsystems, the development was led by LAPAN within Indonesia. Finally, DD refers to a fully autonomous development process conducted entirely by the emerging nation without overseas intervention [22].

3.3.2. Satellite Weight Classification

Satellite weight is used as an indicator of system complexity. Based on internationally adopted classifications, the following four categories which were proposed by Sweeting [23] are used. Satellite weight strongly correlates with the number of subsystems, integration difficulty, required test items (thermal vacuum, vibration, etc.), and the complexity of power and attitude control systems. An increase in satellite mass necessitates not only a larger structural framework but also a corresponding expansion in the number and sophistication of integrated subsystems. For instance, when larger systems are implemented, enhancing attitude control precision often requires the integration of redundant sensors, while elevated power demands necessitate expanded solar arrays and associated deployment mechanisms. Furthermore, as project budgets scale, more stringent safety and reliability standards are imposed, leading to increasingly rigorous testing protocols. Consequently, satellite mass serves as a robust proxy for system complexity. Utilizing this metric as a classification criterion enables an objective and reproducible evaluation of technical maturity across diverse missions. Therefore, it can be used as a reliable indicator of system complexity. This classification enables the objective and reproducible assessment of differences in technical maturity. The rationale for selecting these four levels is based on the small satellite classification method proposed by Professor Matin Sweeting of the University of Surrey. As this classification is widely used today for identifying satellite sizes, we have adopted the same classification in this paper.
Nano-class: 1–10 kg (primarily CubeSats)
Micro-class: 10–100 kg
Small-class: 100–1000 kg
Large-class: 1000+ kg
In the satellite development systems of the target emerging countries, the development systems and satellite weight categories, as defined in Section 3.3.1 and Section 3.3.2, are classified into 16 levels. These levels correspond to the Satellite Technology Ladder (SaTL), as outlined in Table 2.
Furthermore, while satellite weight is employed as a proxy for technological maturity, the recent proliferation of small satellites—particularly in advanced space-faring nations—has driven the development of sophisticated miniaturization technologies, such as integrated antenna array systems. In these contexts, reduced physical scale is a product of technological advancement rather than a lack of capability; therefore, small-scale platforms will increasingly cease to serve as definitive indicators of technical immaturity. However, as this trend toward high-complexity miniaturization is currently in its nascent stages within the satellite programs of emerging nations, the methodology and findings of this study remain fundamentally robust for the current developmental landscape.

3.4. Coding Procedures and Intercoder Reliability

To minimize subjective judgment and enhance reproducibility, a three-stage coding procedure was adopted. In the first stage, two independent coders classified each mission using SaTL rules based solely on documented sources. In the second stage, to avoid convergence bias, they cross-validated classifications for a specific country (Malaysia) without knowing each other’s rationale. Discrepancies were flagged for adjudication. In the third stage, ambiguous cases were jointly reviewed by the research team using triangulation evidence. Inter-coder reliability was assessed using Cowen’s kappa coefficient, yielding κ = 0.75 for development methods and κ = 1.0 for satellite size. Complete agreement was observed for satellite size due to the availability of clear public information. Although there was some variation in the form of support provided by external partners for the development method, overall, these values showed strong agreement and met the recommended standards for qualitative classification research. To ensure transparency and reproducibility, all coding decisions, justifications, and arbitration notes were recorded in a coding log.
As detailed in Section 3.2, data regarding national satellite projects were sourced from public databases [18,19]. Because these databases often lack granular information on development methodologies, we supplemented our dataset with reputable news media and industry reports. However, a notable limitation is that these public-facing sources are susceptible to survivorship bias; consequently, the documented findings may not fully reflect the complexities or failures inherent in the actual state of development.

3.5. Theoretical Background of the 16-Stage Model of Satellite Technology Ladder (SaTL)

SaTL’s 16-stage structure integrates two distinct theoretical dimensions crucial for explaining the progression of satellite development capabilities. The first dimension (Development Method) is based on the widely recognized stepwise development model in technology transfer and capability formation research: “passive procurement → learning-by-doing procurement → joint development → domestically led development.” The four stages—FP1, FP2, JD, and DD—correspond to increasing learning depth and technological autonomy, aligning with absorptive capacity theory [5] and latecomer industrialization model [24].
The second dimension (Weight Class) uses satellite weight as a proxy for system complexity. It is a fundamental principle in aerospace engineering that increasing weight necessitates more subsystems, greater integration demands, and more stringent testing requirements. Therefore, the hierarchy Nano → Micro → Small → Large and above objectively indicates different stages of technological maturity.
This combined 4 × 4, 16-stage model satisfies (1) independence between dimensions, (2) exhaustiveness in covering capability development stages, and (3) consistent progressivity toward higher stages. It precisely captures the subtle differences in initial capability formation and the progression of technological learning that the existing Space Technology Ladder could not express. Therefore, SaTL provides a highly valid analytical framework for theoretically explaining the development of satellite development capabilities.

3.6. Validity, Limitations, and Bias Mitigation

Several methodological safeguards were implemented to address threats to construct, internal, and external validity. Construct validity was reinforced through the explicit operationalization of classification criteria and the triangulation of independent data sources. Internal validity was strengthened by independent coding, high intercoder reliability, transparent adjudication processes, and conservative inclusion rules designed to avoid overestimating national capabilities. External validity was enhanced through the inclusion of a geographically diverse set of emerging spacefaring nations and the use of internationally accepted satellite size categories aligned with global technological trends since 1990.
Nevertheless, limitations remain. Some missions, particularly defense-related projects, lack sufficiently detailed documentation, introducing potential survivorship bias. Additionally, while SaTL captures two core dimensions of satellite capability—engineering complexity and development method—it does not directly measure institutional learning, systems engineering culture, or national absorptive capacity. These limitations are inherent to large comparative research on technology systems but are mitigated through methodological transparency and systematic application of standardized classification rules.

4. Results

This section provides an overview of the empirical trends derived from the time-series plots of all satellite projects in the 16 emerging countries analyzed in this study. The comprehensive SaTL transition graph, constructed from Appendix A, reveals several notable macro-level tendencies in the evolution of satellite development capabilities. The classification of SaTL levels used in this analysis is based on Table 2, whereas the progression and transitions between these levels are illustrated though the time-series figures.

4.1. Countries Where SaTL Rise Slightly (Type 1)

Countries where progress on the Satellite Technology Ladder (SaTL) has stagnated include Nigeria, Algeria and Peru. Nigeria procures satellites from China and the UK-based Surrey Satellite Technology Ltd. (Guildford, UK), but there has been no transition to domestic development. Additionally, the Federal University of Technology Akure (FUTA) developed a CubeSat with support from a Japanese university (Kyutech), though this initiative has not continued. As shown in Figure 1, Nigeria’s SaTL progression remains limited, with only slight increases over time and no sustained advancement toward higher level of domestic capability.
Similarly, Algeria sources satellites from China and Surrey Satellite Technology Ltd., followed by a technical assistance program. However, with support from Surrey, Algeria has begun developing its capabilities domestically and on the way to move transition for domestic satellite development in the future. As shown in Figure 2, this progression is characterized by incremental increases in SaTL levels; however, the trajectory is not strictly monotonic, with some fluctuations observed in later stages.
In Peru’s case, as shown in Figure 3, an initial period of attempting to independently develop small-sized satellites centered around domestic universities occurred in the early 2010s. However, since then, the space program has ceased satellite development. Although Peru’s space agency (CONIDA) has a long history, having been established in 1974, it specializes in satellite data utilization and science. Attempts at satellite development after the 2010s have not been sustained.

4.2. Countries with Rising SaTL (Type 2)

Among the countries where the Satellite Technology Ladder (SaTL) has advanced, Chile, Thailand and Malaysia, have only begun to make significant progress in recent years, despite limited development in the past. As shown in Figure 4, Figure 5 and Figure 6, these countries have had satellites since the 1990s, providing them with an established history in the field; however, until the latter half of the 2010s, their efforts primarily relied on satellite procurement or externally supported development. All of these countries have had satellites since the 1990s, giving them a certain history in the field, but until the latter half of the 2010s, they primarily relied on satellite procurement or externally supported development. Chile has sourced satellites from Surrey Satellite Technology Ltd. and Astrium, while Thailand has procured from American, European, and other international companies, with Malaysia following a similar pattern. However, between the late 2010s and around 2020, these countries have shown a tendency to begin developing satellites using their own technologies, albeit on a smaller scale.
As reflected in Figure 7, Egypt initially procured satellites from European and Ukrainian companies but has since moved towards developing its own CubeSats. Since 2020, Egypt has also started developing medium-sized satellites with support from China. In contrast, Vietnam and the Philippines were late entrants into satellite development, but since 2010, around the time of establishing their respective space agencies, they have strategically aimed to transition to domestic development. Although they are still in the process of developing their own satellites, their focus has been on acquiring technology from abroad, as shown by the later trends in Figure 8 and Figure 9, primarily from Japan.

4.3. Countries’ Industry Expanding After SaTL Rises (Type 3)

Countries expected to expand their satellite development capabilities following the rise of SaTL include Singapore and the UAE. Although relatively late entrants into satellite projects, both countries began making significant strides since around 2010. Singapore established the Office for Space Technology and Industry (OSTIn) in 2013, while the UAE founded the UAE Space Agency in 2014. Since then, both nations have actively introduced foreign technologies and provided support to domestic universities and companies. Despite being latecomers to satellite technology acquisition, both countries have quickly focused on building domestic development capabilities following the establishment of their space agencies (or equivalent offices in Singapore), as evidenced by SaTL progression shown in Figure 10 and Figure 11. Furthermore, the number of stakeholders involved has expanded, with participation growing from companies to universities. In the case of both countries, it is noteworthy that policies aimed at industrial promotion take precedence over those focused on pure science or academic objectives.

4.4. Countries with Higher SaTL Since the Beginning (Type 4)

Countries with higher SaTL than initially expected include Argentina, Iran, Pakistan, South Africa, and Turkiye. These countries vary in terms of when they began satellite development, the size of the satellites they produce, and the nature of their missions, all of which are influenced by their economic conditions and technological capabilities. The SaTL progression shown in Figure 12, Figure 13, Figure 14, Figure 15 and Figure 16 indicates that these countries have pursued domestic development from the outset. While it is possible that they have received foreign technology and support not publicly disclosed, even when collaborating with international companies, these efforts have generally been carried out under national leadership. Some countries, such as Argentina, have consistently pursued independent development, while others, like Turkiye, focus on domestic development but aim to enhance local technological expertise through collaboration with foreign companies. A common characteristic among countries with self-development capabilities may be their association with advanced military technologies.

4.5. Analysis of Satellite Missions Using SaTL

Application of the Satellite Technology Ladder (SaTL) resulted in the classification of 265 satellite missions from 16 emerging spacefaring nations between 1990 and 2024. The distribution of SaTL levels shows a clear concentration of early missions in the lower-left quadrant of the matrix, corresponding to CubeSat-class satellites developed through foreign procurement or externally supported development. Also, only 6.6% of missions reached Levels 15–16, representing indigenous development of small satellites or larger satellites. Countries with multiple universities operating active CubeSat programs—such as Turkiye, Argentina, and South Africa—exhibited significantly higher mission counts, suggesting that academic ecosystems play a central role in early capability accumulation.
A temporal analysis shows a progressive shift from externally supported development to domestically supported and indigenous development over the three decades surveyed. The median SaTL level rose from 6.9 in the early period (1990–2009) to 9.3 in the middle period (2010–2019) and to 10.7 in the most recent period (2019–2024). This upward shift indicates that emerging countries increasingly transition toward more autonomous development practices and larger, more complex satellite platforms.
For each classification from Type 1 to Type 4, a numerical analysis of SaTL was conducted as shown in Table 3. The average values were calculated for each of the following: the average value of SaTL, the number of years required to transition from FP1 to FP2 or JD, the number of years required to transition from the first satellite project to DD, and the increase in weight class among countries that achieved DD.
For Mean SaTL, the average values showed an increasing trend from Type 1 to Type 4. This is a natural result, as Type 4 categorizes countries capable of pursuing independent development from the outset, while Type 1 represents the opposite.
Regarding the number of years to transition from FP1 to FP2/JD, Type 2 took less time than Type 1, while Type 3 took the longest. This is likely because Type 3 countries, being relatively well-funded, implemented FP1 at a fairly early stage, making the transition to the next phase take longer. It is clear that a considerable number of years are required for any Type.
The time required to reach the first DD is clearly shorter for Type 3 than Type 2, though both Type 2 and Type 3 still require considerable time. Type 1 has not reached DD yet.
Regarding DD weight increase, Type 2 again shows a tendency toward less successful scaling up. Type 3 and Type 4 exhibit similar values, indicating that all countries have achieved sizes ranging from CubeSats to microsatellites.

4.6. Analytical Strategy: Cross-National Trajectory Mapping

Once classified, satellite missions were plotted chronologically for each country to visualize technological trajectories. This longitudinal mapping made it possible to identify linear progression, capability leapfrogging facilitated by foreign collaboration, subsystem-specialization pathways, oscillating trajectories, and hybrid models combining academic-led and industry-led development. The analysis used pattern-matching techniques to compare observed trajectories with theoretical expectations derived from the literature on national innovation systems, technological upgrading, and latecomer development. Particular attention was paid to transitions across development methods—especially shifts from externally supported development to domestically supported or indigenous development—as such shifts signify substantial increases in technological autonomy.
In the process of acquiring space technology, particularly satellite technology, emerging countries face numerous challenges, including economic constraints, underdeveloped technological infrastructure such as supply chains, and a limited number of universities and companies with expertise in space technology. However, these challenges can be mitigated by the advantages of adopting technologies already established by developed nations. This approach enables emerging countries to significantly reduce the time required to develop and implement technologies into domestic capability, compared to the extensive periods taken by countries like the United States and the Soviet Union in the history of space development. This two-axis mapping attempts to trace the trajectory of these technological acquisitions.
First, although all countries begin their satellite programs at lower SaTL levels—typically corresponding to procurement-based development of medium- to large-scale satellites—their subsequent trajectories vary markedly. The aggregated plot demonstrates a general downward shift in satellite size over time, reflecting the global diffusion of CubeSats and small satellites as accessible platforms for hands-on technology learning. This shift is particularly pronounced in countries such as Chile, Malaysia, Vietnam, and Thailand, where the appearance of CubeSats coincides with the first observable rise in SaTL levels.
Second, the longitudinal distribution of SaTL values indicates that transitions from procurement-based activities (SaTL Levels 1–4) to external development with foreign support (Levels 5–8) are relatively common among emerging nations. However, upward transitions beyond Levels 8–12—representing domestically executed development with varying degrees of external support—are less frequent and limited to countries with strong institutional or industrial foundations, such as Turkiye, Iran, South Africa, and Argentina. These countries demonstrate not only increased SaTL levels but also broader dispersion across satellite weight classes, suggesting both diversification of development capabilities and expansion of domestic actors involved in satellite projects.
Third, the two-axis diagrams presented in Appendix B (development approach on the X-axis and satellite weight class on the Y-axis) highlight structural patterns that are not immediately visible in SaTL time-series plots alone. Countries with primarily procurement-based programs cluster in the top-left region, whereas those progressing toward independent development consistently shift toward the lower-right region. This movement corresponds to simultaneously adopting smaller satellite platforms for training and increasing the autonomy of development processes. The visualization reinforces the identification of non-linear trajectory groups—some countries exhibit steady, monotonic progression, while others oscillate between development modes depending on partnerships and domestic capacity.
Together, these graphical observations serve as a foundation for the typology presented in the next subsection. They indicate that the evolution of satellite capability acquisition among emerging nations is neither uniform nor strictly incremental. Instead, it reflects a composite of institutional readiness, international collaboration patterns, and the strategic adoption of satellite size as an instrument for phased learning. Building on these empirical insights, the following section classifies the countries into four developmental trajectories that capture these heterogeneous patterns.

5. Discussion

The results of this study reveal substantial diversity in how emerging space nations build satellite capabilities, demonstrating that capability development is shaped by institutional configurations, access to international collaboration, and the presence of domestic industrial structures. Rather than converging on a uniform linear pathway, countries follow a range of developmental trajectories as shown in Appendix B figures, that reflect differences in strategic choices, organizational learning mechanisms, and ecosystem alignment.

5.1. Factors Influencing Trajectory Divergence

Cross-national comparison revealed several structural factors that contribute to divergent SaTL trajectories. Countries that utilize domestic systems enabling collaboration among government agencies, universities, and domestic industry tend to demonstrate more linear and sustained progress in capability development. Institutional stability and continuity of mission, as seen in Argentina and Turkiye, support the gradual accumulation of expertise in subsystems and system engineering capabilities [8,14].
Conversely, nations with fragmented institutional environments or inconsistent funding cycles experience oscillating or plateau patterns. In these contexts, university-led initiatives may dominate early capability-building efforts but fail to translate into sustained industrial or national systems-level capacity.
International technology transfer programs also exert significant influence. Structured partnerships that include long-term training, joint design activities, and hands-on subsystem development—such as the Japanese support programs for the Philippines and Vietnam—facilitate leapfrogging effects by accelerating tacit knowledge acquisition [12]. However, when technology transfer is limited to hardware procurement, the resulting influence on national capability trajectory is minimal.
Finally, domestic industrial participation emerges as a critical determinant of indigenous capability formation. Countries possessing aerospace SMEs or state-owned integrators capable of absorbing transferred technology—such as INVAP in Argentina or TUBITAK UZAY in Turkiye—demonstrate significantly stronger upper range in SaTL trajectories. In contrast, nations lacking such structural complementarities remain dependent on externally supported programs.

5.2. Institutional Ecosystems and International Technology Transfer as a Catalyst

Trajectory divergence is closely linked to the strength of domestic ecosystems. Nations with coordinated university–government–industry structures are more likely to consolidate subsystem knowledge and accumulate higher-level engineering capabilities. In contrast, oscillating or plateau trajectories often arise where such coordination is weak or unstable. These findings echo broader innovation systems scholarship, suggesting that capability-building depends not merely on technical training but also on institutions that retain and deploy accumulated knowledge.
International collaboration plays a catalytic role but is not uniformly transformative. Programs that incorporate hands-on subsystem development, co-design activities, and long-term knowledge exchange contribute meaningfully to upward mobility in SaTL levels. However, procurement-focused or short-duration partnerships rarely embed knowledge deeply enough to shift national trajectories. This highlights the need to distinguish between superficial and substantive forms of technology transfer.

5.3. Implications for Satellite Capability Assessment

The identification of four distinct trajectories challenges the traditional view—common in Technology Ladder literature—that nations progress through standardized, sequential stages. Instead, the evidence supports a more dynamic and path-dependent model of capability formation, aligning with institutionalist perspectives that emphasize complementarities between organizational routines, policy environments, and learning structures. Leapfrogging cases, in particular, highlight the nonlinearity of technological upgrading and suggest that targeted international partnerships can accelerate absorptive capacity under the right institutional conditions.
By capturing the interaction between engineering complexity and development autonomy, SaTL provides an analytical lens that makes visible the subtle transitions that existing national-level frameworks overlook. The framework’s granularity clarifies how early CubeSat programs act as capability incubators but require institutional reinforcement and industrial integration to translate into sustained progress. This diagnostic capability positions SaTL as a useful tool for policymakers seeking to design more effective capability-building strategies.

6. Conclusions

6.1. Summary

This study demonstrates the value of a project-level analytical framework for understanding how emerging nations develop satellite capabilities. By introducing the Satellite Technology Ladder (SaTL) and applying it to a multi-country dataset of 265 satellite missions, the research offers a structured means of comparing technological development paths across diverse national contexts. SaTL’s integration of development autonomy and engineering complexity allows for clearer identification of capability transitions and provides explicit features for describing national trajectories.
The study’s primary contribution lies in offering a replicable methodology and a nuanced conceptual tool for evaluating capability formation beyond coarse national indicators. The typology of trajectories generated through SaTL analysis provides policymakers with actionable insights into how institutional stability, industrial participation, and structured technology transfer shape national advancement. The findings also extend theoretical discussions on latecomer innovation by highlighting the role of nonlinearity, knowledge retention, and ecosystem alignment in enabling or constraining strategic technological upgrading.

6.2. Limitation

While the study relies on publicly available information and focuses primarily on satellite engineering dimensions, future research can expand SaTL to incorporate organizational, regulatory, or systems-engineering factors. Drawing upon Technology Ladder theory, this study examines the trajectory of satellite development in emerging nations, with a dual focus on development methodologies and size. While the proposed 16-step framework provides a structured taxonomy based on these two axes, it is important to clarify that this model does not imply an inevitable linear progression. Despite its streamlined nature, the framework remains a robust analytical tool for categorizing and discussing the discrete stages of national space capacity building. Furthermore, longitudinal case studies, interviews with practitioners, and quantitative analyses of transition probabilities represent promising next steps. Ultimately, this research lays the groundwork for a comprehensive, evidence-based approach to understanding and guiding capability development in the global space sector.
Drawing upon Technology Ladder theory, this study examines the mechanisms through which emerging nations can accelerate technology acquisition, with a particular emphasis on international technology transfer. While this research categorizes various models of international collaborative projects, a critical next step is to analyze empirical case studies to evaluate how specific project-level mechanisms—such as human resource development and in-orbit operations—facilitate organizational and technical learning.

6.3. Future Prospects

6.3.1. Refinement and Expansion of the SaTL Framework

While the current SaTL model provides a granular 16-level taxonomy for assessing technological maturity, significant potential exists to broaden its analytical scope. Future research should aim to integrate institutional and absorptive capacity by incorporating metrics that quantify the structural foundations of national space programs. Such metrics might include the density of domestic supply chains, the annual cohort of specialized aerospace graduates, and the stability of long-term fiscal commitments. Accounting for these variables would provide a more holistic assessment of a nation’s long-term aerospace sustainability.

6.3.2. Policy Implications for Sustainable Capacity Building

The findings of this study underscore that technology transfer is a non-linear process, heavily contingent upon domestic institutional strength. Consequently, future policy frameworks for emerging nations should: (1) Prioritize Knowledge Internalization: Transition from “turnkey” procurement models (FP1) toward Joint Development (JD) and Domestic Development (DD). (2) Foster Tacit Knowledge Transfer: Emphasize collaborative frameworks that facilitate the internalization of complex technical expertise rather than mere hardware acquisition.

Author Contributions

Investigation, Methodology, T.F. and N.M.; Validation, E.S. and R.S.I.A.; Data curation, T.F., E.S. and R.S.I.A.; Writing—original draft preparation, T.F.; writing—review and editing, T.F. and N.M.; visualization, T.F.; supervision, N.M.; project administration, T.F.; funding acquisition, T.F. and N.M. All authors have read and agreed to the published version of the manuscript.

Funding

This research was funded by Japan Society for the Promotion of Science JSPS KAKENHI Grant Number 24 K05084.

Data Availability Statement

The data presented in this study are available on request from the corresponding author due to the research currently being conducted.

Acknowledgments

The authors express gratitude to the members of Minato laboratory of Ritsumeikan University graduate school of technology management for their comments.

Conflicts of Interest

The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Abbreviations

The following abbreviations are used in this manuscript:
NASANational Aeronautics and Space Administration
ESAEuropean Space Agency
JAXAJapan Aerospace Exploration Agency
STLSpace Technology Ladde
SaTLSatellite Technology Ladder
GNSSGlobal Navigation Satellite System
LEOLow Earth Orbit
GEOGeostationary Earth Orbit

Appendix A. List of Satellite Projects in Each Country

Table A1. Nigeria.
Table A1. Nigeria.
YearEventMissionSizeWeightStyleSTLPartner
1999NATIONAL SPACE RESEARCH AND DEVELOPMENT AGENCY (NASRDA)National space agency established
2003NigeriaSat 1Earth Observation100 kg212Surrey Satellite Technology (SSTL)
2007NIGCOMSAT 1Communication5150 kg414China Academy of Space Technology (CAST)
2011NigeriaSat 2Earth Observation300 kg313Surrey Satellite Technology (SSTL)
2011NX (NigeriaSat X)Training, Earth Observation100 kg226Surrey Satellite Technology (SSTL)
2011NIGCOMSAT 1RCommunication5150 kg414China Academy of Space Technology (CAST)
2017EduSat 1 (Bird N)Technology, educationCubeSat (1U)125Kyushu Institute of Technology (Kyutech)
Table A2. Algeria.
Table A2. Algeria.
YearEventMissionSizeWeightStyleSTLPartner
2002Algerian Space AgencyEstablished to develop Space programs and technology
2002AlSat 1Earth observation90 kg226Surrey Satellite Technology (SSTL)
2010AlSat 2AEarth observation116 kg327EADS Astrium (Paris, France)
2016AlSat 1BEarth observation103 kg3311Surrey Satellite Technology (SSTL)
2016AlSat 2BEarth observation110 kg3311EADS Astrium
2016AlSat-Nano (AlSat 1N)TechnologyCubeSat (3U)139Surrey Space Centre, UK Space Agency
2017Alcomsat 1Communication5225 kg414China Association for Science and Technology (CAST)
Table A3. Chile.
Table A3. Chile.
YearEventMissionSizeWeightStyleSTLPartner
1995FASat AlfaEarth observation, technology55 kg226Surrey Satellite Technology Ltd. (SSTL)
1998FASat BravoEarth observation, technology55 kg226Surrey Satellite Technology Ltd. (SSTL)
2011SSOT (FASat Charlie)Earth observation117 kg327EADS Astrium
2017SUCHAITechnology, educationCubeSat (1U)1413
2019National Satellite System (SNSat)National satellite constellation for Scientific and technological development to national defense and civil society
2022SUCHAI-2Technology, educationCubeSat (3U)1413
2022SUCHAI-3Technology, educationCubeSat (3U)1413
2022PlantSatTechnology, educationCubeSat (3U)1413
2023FASat Delta (Runner 1)Earth observation86 kg212Tyvak (Irvine, CA, USA), ImageSat International (ISI) (Tel Aviv, Israel)
Table A4. Thailand.
Table A4. Thailand.
YearEventMissionSizeWeightStyleSTLPartner
1993Thaicom 1 → Thaicom 1ACommunication1080 kg (launch); 414Hughes Space and Communications Company (Los Angels, CA, USA)
1994Thaicom 2Communication1080 kg (launch); 414Hughes Space and Communications Company
1997Thaicom 3Communication2652 kg, 414Arianespace (Paris, France)
1998TMSat 1 (TMSat-OSCAR 31, TO 31) → Thai-Paht 1Technology55 kg226Surrey Satellite Technology Ltd. (SSTL)
2000Thai Ministry of Science and Technology Space Agency (GISTDA) Established, Responsible for space technology and geo-informatics applications
2005iPStar 1 (Thaicom 4, MEASAT 5, Synertone 1)Communication6505 kg, 3400 kg (dry)414Space Systems/Loral (SS/L) (Palo Alto, CA, USA)
2006Thaicom 5 (ex Agrani 2 ex Thaicom 4)Communication2652 kg, 414Arianespace
2008THEOS 1 (Thaichote)Earth Observation750 kg327Astrium (Paris, France)
2014Thaicom 6 (AfriCom 1)Communication3016 kg414Orbital Sciences Corporation (OSC) (Dulles, VA)
2016Thaicom 8 Communication3025 kg414Orbital Sciences Corporation (OSC)
2018KNACKSATTechnologyCubeSat (1U)1413
2019JAISAT 1TechnologyCubeSat (3U)1413
2020NAPA 1 (RTAF-SAT 1)Technology, earth observationCubeSat (6U)111ISISPACE (Delft, Netherland)
2021BCCSAT 1TechnologyCubeSat (1U)1413
2021NAPA 2 (RTAF-SAT 2)Technology, earth observationCubeSat (6U)111ISISPACE
2023THEOS 2Earth Observation450 kg327Airbus (Toulouse, France)
2023LOGSATSCommunications IoTCubeSat (3U)1413
Table A5. Malaysia.
Table A5. Malaysia.
YearEventMissionSizeWeightStyleSTLPartner
1996MEASAT 1 → Africasat 1Communication1450 kg 414Hughes Space and Communications International, Inc. (HSCI)
1996MEASAT 2 → Africasat 2Communication1450 kg414Hughes Space and Communications International, Inc. (HSCI)
2000TiungSat 1 (MySat 1, Malaysian-OSCAR 46, MO 46)Earth observation, technologyMicrosat-70226Surrey Satellite Technology (SSTL)
2002National Space Agency (ANGKASA)Legislate policy and rules, coordinate, implement and monitor space activities.
2006MEASAT 3Communication4765 kg414Hughes Space and Communications International, Inc. (HSCI)
2009MEASAT 3aCommunication2367 kg414Orbital Sciences Corporation (OSC)
2009RazakSAT (ex MACSAT) Earth observation200 kg327Satrec Initiative (SATRECI)
2014MEASAT 3b (Jabiru 2)Communication5897 kg414EADS Astrium → Airbus Defence and Space (Taufkirchen, Germany)
2018UiTMSAT 1 (Bird MYS)Technology, educationCubeSat (1U)125Kyushu Institute of Technology (Kyutech)
2018InnoSat 2 TechnologyCubeSat (3U)1413
2019Malaysian Space Agency (MYSA)Merging of Malaysian Remote Sensing Agency (MRSA) and National Space Agency (ANGKASA).
2022MEASAT 3dCommunication5648 kg414Airbus Defence and Space
2023A-SEANSAT-PG 1 Traffic monitoring, earth observationCubeSat (6U)1413
2023SpaceANT-D Communications (IoT)PocketQube (1P)1413
Table A6. Vietnam.
Table A6. Vietnam.
YearEventMissionSizeWeightStyleSTLPartner
2005Vietnam Posts and Telecommunications Group
(VNPT) started space programs
Launching telecommunications satellite
2008VINASAT 1Communication2637 kg414Lockheed Martin (Bethesda, MD, USA) and Telesat Satellite Operator (Ottawa, ON, Canada)
2011Vietnam National Satellite Center (VNSC)Manage, and implement the Vietnam Space Center project
2012VINASAT 2Communication2969 kg414Lockheed Martin and Telesat Satellite Operator
2012F1TechnologyCubeSat (1U)1413
2013VNREDSat 1aEarth observation115 kg327EADS Astrium
2013PicoDragonTechnologyCubeSat (1U)1413
2019MicroDragonTechnology50 kg226Tohoku University, University of Tokyo, Hokkaido University, Keio University, and Kyushu Institute of Technology
2021NanoDragonTechnologyCubeSat (3U)1413
Table A7. Philippines.
Table A7. Philippines.
YearEventMissionSizeWeightStyleSTLPartner
1997Agila 2/ABS 5 → ABS 3Communication3775 kg (launch); 414Space Systems/Loral (SS/L)
2016DIWATA-1Earth observation50 kg 226Hokkaido University and Tohoku University
2018Maya-1Technology, educationCubeSat (1U)125Kyushu Institute of Technology (Kyutech)
2018Diwata 2Earth observation56 kg226Hokkaido University and Tohoku University
2019Philippine Space Agency (PhilSA)Established to address all national issues and activities related to space science and technology applications
2021Maya-2Technology, educationCubeSat (1U)125Kyushu Institute of Technology (Kyutech)
2021Maya-3,4Technology, educationCubeSat (1U)1413
2023Maya-5,6cubesatCubeSat (1U)1413
Table A8. Egypt.
Table A8. Egypt.
YearEventMissionSizeWeightStyleSTLPartner
1998Nilesat 101Communication1827 kg414Astrium
2000Nilesat 102Communication1827 kg414Astrium
2007EgyptSat 1 (MisrSat 1)Earth Observation, Technology160 kg327Yuzhnoye (Dnipro, Ukraine)
2010Nilesat 201Communication3200 kg414Thales Alenia Space
2014EgyptSat 2 (MisrSat 2)Earth Observation1050 kg428RSC Energia (Korolyov, Russia)
2018Egyptian Space AgencyTo build satellites and launch them from Egyptian territories
2019EgyptSat A (MisrSat A)Earth Observation~1000 kg427RKK Energiya (Korolyov, Russia)
2019NARSScube 2TechnologyCubeSat (1U)1413
2019NARSScube 1 (ex Egycubesat 1)TechnologyCubeSat (1U)1413
2019Tiba 1Communication, military5640 kg414Thales Alenia Space (Cannes, France), Airbus Defence and Space
2022Nilesat 301Communication3938 kg414Thales Alenia Space
2023Horus 1 (Helusi 1)Earth Observation~300 kg327Chinese company DFH (Beijin, China)
2023Horus 2 (Helusi 2)Earth Observation>300 kg327Chinese company DFH
2023MisrSat 2 (Egypt 2, Aiji 2)Earth Observation350 kg3311CAST
2024NExSat 1Technology, Earth observation65 kg2414
Table A9. Singapore.
Table A9. Singapore.
YearEventMissionSizeWeightStyleSTLPartner
1998ST 1Communication3200 kg414Astrium
2011X-SatEarth Observation, Technology105 kg3311Satrec Initiative Ltd. (Daejeon, South Korea)
2011ST 2Communication5090 kg414Mitsubishi Electric (MELCO) (Tokyo, Japan)
2013Established the Office for Space Technology and Industry (OSTIn)Build a thriving space industry for Singapore.
2013VELOX P2TechnologyCubeSat (1U)1413
2014ABS 2 (ST 3, Koreasat 8)Communication6330 kg414Space Systems/Loral (SS/L)
2014POPSAT-HIP 1TechnologyCubeSat (3U)1113
2014VELOX 1 (VELOX 1-NSAT)TechnologyCubeSat (3U)1413
2014VELOX P3 (VELOX 1-PSAT)Technology0.25 kg1413
2015GalassiaTechnologyCubeSat (2U)1413
2015Athenoxat 1TechnologyCubeSat (3U)1413
2015Kent Ridge 1 (KR 1)Earth Observation78 kg226Berlin Space Technologies (Berlin, Germany), TU (Technical University) Berlin
2015VELOX C1Technology123 kg3415
2015TeLEOS 1Earth Observation400 kg3415
2015VELOX 2TechnologyCubeSat (6U)1413
2016AOBA-VELOX 3TechnologyCubeSat (2U)125Kyushu Institute of Technology (Kyutech)
2018SpatiumIonospheric research, TechnologyCubeSat (2U)125Kyushu Institute of Technology (Kyutech)
2019AOBA-VELOX 4TechnologyCubeSat (2U)139Kyushu Institute of Technology (Kyutech)
2019SpooQy 1TechnologyCubeSat (3U)1413
2019JCSat 18/Kacific 1Communication6956 kg414Boeing (Crystal City, VA, USA)
2021NuX 1TechnologyCubeSat (3U)1413
2022NeuSAREarth Observation, radar155 kg3311Satrec Initiative (SATRECI), MMA Design (Broomfiels, CO, USA)
2022DS-EOEarth Observation365 kg3415
2022SCOOB 1 (S3 1)TechnologyCubeSat (3U)1413
2023Zeus 1TechnologyCubeSat (3U)1413
2023Lumelite 4Technology, communicationsCubeSat (12U)2414
2023TeLEOS 2Earth Observation, radar750 kg3415
2023NuLIoNCommunications, technologyCubeSat (3U)139NuSpace (Singapore)
2023DS-SAREarth Observation, radar352 kg314IAI (Israel Aerospace Industries) (Lod, Israel)
2023ARCADE (INSPIREsat 4)Technology24 kg2414
2023Galassia 2TechnologyCubeSat (3U)1413
2023SCOOB 2 (S3 2)TechnologyCubeSat (3U)1413
2023VELOX AMTechnology23 kg2414
Table A10. UAE.
Table A10. UAE.
YearEventMissionSizeWeightStyleSTLPartner
2000Thuraya 1Communication5108 kg414Boeing
2003Thuraya 2Communication5177 kg414Boeing
2008Thuraya 3 Communication5177 kg414Boeing
2009DubaiSat 1Earth Observation, Technology~200 kg327Satrec Initiative (SATRECI)
2011YahSat 1A (Y1A) → Al Yah 1Communication5965 kg414EADS Astrium
2012YahSat 1B (Y1B) → Al Yah 2Communication6100 kg414EADS Astrium
2013DubaiSat 2Earth Observation, Technology~300 kg327Satrec Initiative (SATRECI)
2014UAE SPACE AGENCYRaise awareness of the importance of the Space sector and the development of the qualified human resources in the Space field
2017Nayif 1Technology, educationCubeSat (1U)1413
2018Al Yah 3 (AY 3)Communication3795 kg414Orbital ATK (Dulles, VA, USA)
2018KhalifaSat (DubaiSat 3)Earth Observation, Technology330 kg3415
2018MYSAT 1Technology, educationCubeSat (1U)1413
2020Al-Amal (Hope, Emirates Mars Mission, EMM)Mars orbiter1350 kg4312Laboratory for Atmospheric and Space Physics, at the University of Colorado at Boulder (LASP)
2020MeznSatEarth observationCubeSat (3U)1413
2020Falcon Eye 2Reconnaissance, optical1190 kg414Airbus Defence and Space (prime), Thales Alenia (payload)
2021MYSAT 2 (DhabiSat)Technology, educationCubeSat (2U)1413
2021DMSat 1Earth observation15 kg226University of Toronto Institute for Aerospace Studies
2021GhalibTechnologyCubeSat (2U)111ISISpace (prime); Marshall Intech (payload) (Dubai, UAE)
2021Light 1Earth observationCubeSat (3U)1413
2022DEWA-Sat 1CommunicationsCubeSat (3U)1413
2023Sharjah-Sat 1TechnologyCubeSat (3U)1413
2023DEWA-Sat 2Earth observationCubeSat (3U)1413
Table A11. Argentina.
Table A11. Argentina.
YearEventMissionSizeWeightStyleSTLPartner
1990LUSAT (LO 19, LUSAT-OSCAR 19)Amateur radio communication14 kg2414
1991National Space Activities Commission (CONAE)Space efforts towards civilian objectives
1996MuSat 1 (Victor) Technology32 kg2414
1996SAC B Scientific181 kg3415
1997Nahuel 1A Communication1790 kg414Dornier Satellitensysteme (prime) (Friedrichshafen, Germany), Aerospatiale (bus) (Paris, France)
1998SAC A Experimental, Earth observation268 kg3415
2000SAC CScientific485 kg3311NASA, Denmark, INPE, Italy
2002LatinSat A Communication M2M/IoT12 kg212SpaceQuest (Fairfax, VA, USA)
2002LatinSat B Communication M2M/IoT12 kg212SpaceQuest
2007PehuenSat 1 (PO 53, PehuenSat-OSCAR 63) Technology6 kg1413
2011Aquarius/SAC D (ESSP 6)Earth Science (Ocean salinity)1350 kg4312NASA (payload)
2013CubeBug 1 (El Capitán Beto) TechnologyCubeSat (2U)1413
2013CubeBug 2 (Manolito, LO 74, LUSAT-OSCAR 74) TechnologyCubeSat (2U)1413
2014BugSat 1 (Tita) Technology, earth observation22 kg2414
2014ARSAT 1 Communication2985 kg4312Thales Alenia Space (payload)
2015ARSAT 2 Communication2975 kg4312Thales Alenia Space (payload)
2016ÑuSat 1 (NewSat 1, Aleph-1 1, Fresco, Lusat-OSCAR 87, LO 87)Earth observation37.5 kg2414
2016ÑuSat 2 (NewSat 2, Aleph-1 2, Batata) Earth observation37.5 kg2414
2017ÑuSat 3 (NewSat 3, Aleph-1 3, Milanesat)Earth observation37.5 kg2414
2018ÑuSat 4 (NewSat 4, Aleph-1 4, Ada) Earth observation37.5 kg2414
2018ÑuSat 5 (NewSat 5, Aleph-1 5, Maryam) Earth observation37.5 kg2414
2018SAOCOM 1A Earth observation, radar~3000 kg4416
2020SAOCOM 1B Earth observation, radar~3000 kg4416
2020ÑuSat 6 (NewSat 6, Aleph-1 6, Hypatia) Earth observation37.5 kg2414
2020ÑuSat 7 (NewSat 7, Aleph-1 7, Sophie) Earth observation37.5 kg2414
2020ÑuSat 8 (NewSat 8, Aleph-1 8, Marie) Earth observation37.5 kg2414
2020ÑuSat 9 (NewSat 9, Aleph-1 9, Alice) Earth observation41 kg2414
2020ÑuSat 10 (NewSat 10, Aleph-1 10, Caroline) Earth observation41 kg2414
2020ÑuSat 11 (NewSat 11, Aleph-1 11, Cora) Earth observation41 kg2414
2020ÑuSat 12 (NewSat 12, Aleph-1 12, Dorothy) Earth observation41 kg2414
2020ÑuSat 13 (NewSat 13, Aleph-1 13, Emmy) Earth observation41 kg2414
2020ÑuSat 14 (NewSat 14, Aleph-1 14, Hedy) Earth observation41 kg2414
2020ÑuSat 15 (NewSat 15, Aleph-1 15, Katherine) Earth observation41 kg2414
2020ÑuSat 16 (NewSat 16, Aleph-1 16, Lise) Earth observation41 kg2414
2020ÑuSat 17 (NewSat 17, Aleph-1 17, Mary) Earth observation41 kg2414
2020ÑuSat 18 (NewSat 18, Aleph-1 18, Vera) Earth observation41 kg2414
2021DIY 1 (ArduiQube, DO 111, DIY-OSCAR 111) TechnologyPocketQube (1P)1413
2021ÑuSat 19 (NewSat 19, Aleph-1 19, Rosalind) Earth observation37.5 kg2414
2021ÑuSat 20 (NewSat 20, Aleph-1 20, Grace) Earth observation37.5 kg2414
2021ÑuSat 21 (NewSat 21, Aleph-1 21, Elisa) Earth observation37.5 kg2414
2021ÑuSat 22 (NewSat 22, Aleph-1 22, Sofya) Earth observation37.5 kg2414
2022MDQube-SAT 1 (MDQSAT 1, General San Martin) TechnologyPocketQube (2P)1413
2022ÑuSat 23 (NewSat 23, Aleph-1 23, Annie Maunder) Earth observation37.5 kg2414
2022ÑuSat 24 (NewSat 24, Aleph-1 24, Kalpana Chawla) Earth observation37.5 kg2414
2022ÑuSat 25 (NewSat 25, Aleph-1 25, Mária Telkes) Earth observation37.5 kg2414
2022ÑuSat 26 (NewSat 26, Aleph-1 26, Mary Somerville) Earth observation37.5 kg2414
2022ÑuSat 27 (NewSat 27, Aleph-1 27, Sally Ride) Earth observation37.5 kg2414
2022ÑuSat 28 (NewSat 28, Aleph-1 28, Alice Lee) Earth observation37.5 kg2414
2022ÑuSat 29 (NewSat 29, Aleph-1 29, Edith Clarke) Earth observation37.5 kg2414
2022ÑuSat 30 (NewSat 30, Aleph-1 30, Margherita Hack) Earth observation37.5 kg2414
2022ÑuSat 31 (NewSat 31, Aleph-1 31, Ruby Payne-Scott) Earth observation37.5 kg2414
2023ÑuSat 32 (NewSat 32, Aleph-1 32, Albania 1) Earth observation37.5 kg2414
2023ÑuSat 33 (NewSat 33, Aleph-1 33, Albania 2) Earth observation37.5 kg2414
2023ÑuSat 34 (NewSat 34, Aleph-1 34, Amelia Earhart) Earth observation37.5 kg2414
2023ÑuSat 35 (NewSat 35, Aleph-1 35, Williamina Fleming) Earth observation37.5 kg2414
2023ÑuSat 36 (NewSat 36, Aleph-1 36, Annie Jump Cannon) Earth observation37.5 kg2414
2023ÑuSat 37 (NewSat 37, Aleph-1 37, Joan Clarke) Earth observation37.5 kg2414
2023ÑuSat 38 (NewSat 38, Aleph-1 38, Maria Gaetana Agnesi) Earth observation37.5 kg2414
2023ÑuSat 39 (NewSat 39, Aleph-1 39, Tikvah Alper) Earth observation37.5 kg2414
2023ÑuSat 40 (NewSat 40, Aleph-1 40, Carolyn Shoemaker) Earth observation37.5 kg2414
2023ÑuSat 41 (NewSat 41, Aleph-1 41, Cecilia Payne-Gaposchkin) Earth observation37.5 kg2414
2023ÑuSat 42 (NewSat 42, Aleph-1 42, María Wonenburger) Earth observation37.5 kg2414
2023ÑuSat 43 (NewSat 43, Aleph-1 43, Rose Dieng-Kuntz) Earth observation37.5 kg2414
2023MDQSAT 1C TechnologyCubeSat (0.5U)1413
2023MDQSAT 1D TechnologyCubeSat (0.5U)1413
2023MDQube-SAT 2 TechnologyPocketQube (2P)1413
2024ÑuSat 44 (NewSat 44, Aleph-1 44, Maria Mitchell) Earth observation37.5 kg2414
Table A12. Iran.
Table A12. Iran.
YearEventMissionSizeWeightStyleSTLPartner
2004Iran’s Space Agency (ISA)Peaceful applications of space science and technology
2005Sina 1Technology160 kg313NPO Polyot (Omsk, Russia)
2009OmidTechnology27 kg2414
2011Rasad 1Earth observation, Technology15 kg2414
2012NavidEarth observation50 kg2414
2015FajrTechnology52 kg2414
2017Toloo 1Earth observation100 kg2414
2019Payam-e Amirkabir (AUTSAT 1, Amir-Kabir 1)Earth observation, store and forward communications90 kg2414
2019Dousti 1Earth observation52 kg2414
2020Zafar 1Earth observation113 kg3415
2020Noor 1MilitaryCubeSat (6U)1413
2021Toloo 2(Toloo 1 copy) Earth observation100 kg2414
2022Noor 2MilitaryCubeSat (6U)1413
2022Khayyam 1Earth observation600 kg313All-Russian Scientific Research Institute of Electromechanics (VNIIEM)
2023Nahid 1Communications50 kg2414
2023Noor 3MilitaryCubeSat (6U)1413
2024SurayaCommunications50 kg2414
2024Hatef 1TechnologyCubeSat (3U)1413
2024Kaihan 2TechnologyCubeSat (3U)1413
2024MehdaTechnology32 kg2414
2024Pars 1Earth observation, Communications134 kg3415
2024Nahid 2Communications110 kg3415
Table A13. Pakistan.
Table A13. Pakistan.
YearEventMissionSizeWeightStyleSTLPartner
1990Badr ATechnology52 kg2414
1991SUPARCO and the Chinese Ministry of Aerospace Industry signed an agreementStrengthen space cooperation
2001Badr BTechnology68.5 kg2414
2011PakSAT 1RCommunication5120 kg414China Association for Science and Technology (CAST)
2013ICUBE 1TechnologyCubeSat (1U)1413
2018PakTES 1A Earth observation300 kg3415
2018PRSS 1Earth observation1200 kg444
2024PakSAT-MM 1Communication5400 kg414China Association for Science and Technology (CAST)
2024ICUBE QLunar orbiter, technology7 kg1413
Table A14. South Africa.
Table A14. South Africa.
YearEventMissionSizeWeightStyleSTLPartner
1999Sunsat (SO 35, Sunsat-OSCAR 35)Experimental63 kg2414
2009Sumbandila (ZA-002, SO 67, SumbandilaSat
-OSCAR 67)
Experimental81 kg2414
2010South African National Space Agency (SANSA) Established to promote the use of space and cooperation in space-related activities
2013ZACUBE 1 (TshepisoSat, ZA 003)TechnologyCubeSat (1U)1413
2014Kondor-EEarth observation, radar1100 kg414NPO Mashinostroyeniya (Reutov, Russia)
2017nSIGHT 1 (QB50 AZ02)Technology, atmosphere, earth observationCubeSat (2U)1413
2017ZA-AeroSat (QB50 AZ01)Technology, atmosphereCubeSat (2U)1413
2018ZACUBE 2 (ZA 004)TechnologyCubeSat (3U)1413
2022MDASat 1a, 1b, 1cTechnology, Satellite constellationCubeSat (2U)1413
2023EOS-SAT 1 (EOS Agrisat-1)Earth observation178 kg3415
Table A15. Turkiye.
Table A15. Turkiye.
YearEventMissionSizeWeightStyleSTLPartner
1994Türksat 1ACommunication1743 kg4312Aerospatiale
1994Türksat 1BCommunication1743 kg4312Aerospatiale
1996Türksat 1CCommunication1743 kg4312Aerospatiale
2001Eurasiasat 1 (Türksat 2A)Communication3535 kg428Alcatel Space (Cannes, France)
2003Bilsat 1Earth Observation130 kg327SSTL
2008Türksat 3ACommunication3110 kg428Alcatel Alenia Space (Cannes, France)
2009ITÜ-pSat 1TechnologyCubeSat (1U)1413
2011RASATEarth Observation95 kg2414
2012Göktürk 2Reconnaissance, optical450 kg3415
2013TurkSat-3USatTechnology, CommunicationCubeSat (3U)1413
2014Türksat 4ACommunication4850 kg428Mitsubishi Electric MELCO
2015Türksat 4BCommunication4924 kg428Mitsubishi Electric MELCO
2016Göktürk 1AReconnaissance, optical1060 kg4312Telespazio (Rome, Italy)
2017BeEagleSat (QB50 TR01)Technology, atmospheric scienceCubeSat (2U)1413
2017HAVELSAT (QB50 TR02)Technology, atmospheric scienceCubeSat (2U)1413
2018Turkish Space Agency (TUA)Space exploration
2018UBAKUSAT (UBAK-3U-SAT)Technology, communicationCubeSat (3U)1413
2021Türksat 5ACommunication3500 kg428Airbus Defence and Space
2021ASELSATTechnologyCubeSat (3U)1413
2021Türksat 5BCommunication4500 kg428Airbus Defence and Space
2022Grizu-263aTechnologyPocketQube (1P)1413
2022Connecta T1.1Technology, communicationsCubeSat (3U)1413
2023Connecta T1.2Technology, communicationCubeSat (3U)1413
2023Connecta T2.1Technology, communication, earth observationCubeSat (6U)1413
2023İmeceEarth Observation800 kg3415
2023KILIÇSATTechnologyCubeSat (6U)1413
2023IstanbulTechnologyPocketQube (1P)1413
2023Hello Test 1, 2Technology, communications (IoT)PocketQube (2P)1413
2023Connecta T3.1Technology, communication, earth observationCubeSat (6U)1413
2023Connecta T3.2Technology, communication, earth observationCubeSat (6U)1413
2024Türksat 6ACommunication4250 kg4416
Table A16. Peru.
Table A16. Peru.
YearEventMissionSizeWeightStyleSTLPartner
1974National Commission for Aerospace Research and Development (CONIDA) establishedLead agency for all space activities
2013PUCP-Sat 1Deploy the 127 g Pocket-PUCP picosatelliteCubeSat (1U)1413
2013Pocket-PUCPTechnology127 g3413
2014Chasqui 1Technology, educationCubeSat (1U)139Russian Southwest State University (SWSU)
2014UAPSat 1Technology, educationCubeSat (1U)1413
2016PerúSat 1Earth observation430 kg3415
2023Andesat 1, 2CommunicationsUnder 400 kg313Astranis (San Francisco, CA, USA)

Appendix B. Development Phase and Satellite Weight Class Axis Graphs

1.
Overseas Procurement Model
Figure A1. Curved trajectory of Algeria.
Figure A1. Curved trajectory of Algeria.
Aerospace 13 00330 g0a1
Figure A2. Curved trajectory of Nigeria.
Figure A2. Curved trajectory of Nigeria.
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2.
Overseas Technology Introduction Model
Figure A3. Curved trajectory of Chile.
Figure A3. Curved trajectory of Chile.
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Figure A4. Curved trajectory of Thailand.
Figure A4. Curved trajectory of Thailand.
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Figure A5. Curved trajectory of Vietnam.
Figure A5. Curved trajectory of Vietnam.
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Figure A6. Curved trajectory of Malaysia.
Figure A6. Curved trajectory of Malaysia.
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Figure A7. Curved trajectory of Egypt.
Figure A7. Curved trajectory of Egypt.
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3.
Overseas Collaboration model
Figure A8. Curved trajectory of Singapore.
Figure A8. Curved trajectory of Singapore.
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Figure A9. Curved trajectory of UAE.
Figure A9. Curved trajectory of UAE.
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4.
Domestic Development Model
Figure A10. Curved trajectory of Argentina.
Figure A10. Curved trajectory of Argentina.
Aerospace 13 00330 g0a10
Figure A11. Curved trajectory of Iran.
Figure A11. Curved trajectory of Iran.
Aerospace 13 00330 g0a11
Figure A12. Curved trajectory of Pakistan.
Figure A12. Curved trajectory of Pakistan.
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Figure A13. Curved trajectory of Turkiye.
Figure A13. Curved trajectory of Turkiye.
Aerospace 13 00330 g0a13
Figure A14. Curved trajectory of South Africa.
Figure A14. Curved trajectory of South Africa.
Aerospace 13 00330 g0a14
Figure A15. Curved trajectory of Peru.
Figure A15. Curved trajectory of Peru.
Aerospace 13 00330 g0a15

References

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Figure 1. SaTL of Nigeria.
Figure 1. SaTL of Nigeria.
Aerospace 13 00330 g001
Figure 2. SaTL of Algeria.
Figure 2. SaTL of Algeria.
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Figure 3. SaTL of Peru.
Figure 3. SaTL of Peru.
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Figure 4. SaTL of Chile.
Figure 4. SaTL of Chile.
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Figure 5. SaTL of Thailand.
Figure 5. SaTL of Thailand.
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Figure 6. SaTL of Malaysia.
Figure 6. SaTL of Malaysia.
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Figure 7. SaTL of Egypt.
Figure 7. SaTL of Egypt.
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Figure 8. SaTL of Vietnam.
Figure 8. SaTL of Vietnam.
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Figure 9. SaTL of Philippines.
Figure 9. SaTL of Philippines.
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Figure 10. SaTL of Singapore.
Figure 10. SaTL of Singapore.
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Figure 11. SaTL of UAE.
Figure 11. SaTL of UAE.
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Figure 12. SaTL of Argentina.
Figure 12. SaTL of Argentina.
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Figure 13. SaTL of Iran.
Figure 13. SaTL of Iran.
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Figure 14. SaTL of Pakistan.
Figure 14. SaTL of Pakistan.
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Figure 15. SaTL of South Africa.
Figure 15. SaTL of South Africa.
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Figure 16. SaTL of Turkiye.
Figure 16. SaTL of Turkiye.
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Table 1. Target Countries.
Table 1. Target Countries.
RegionCountry
South AmericaArgentina, Chile, Peru
AsiaPhilippines, Vietnam, Malaysia, Thailand,
Pakistan, Singapore
Middle EastUAE, Iran, Turkiye
AfricaEgypt, Nigeria, Algeria, South Africa
Table 2. Satellite Technology Ladder (SaTL).
Table 2. Satellite Technology Ladder (SaTL).
Development MethodSatellite SizeSaTL
1. Procurement + Training (FP1)1. Nano satellites1
2. Micro satellites2
3. Small satellites3
4. Large satellites4
2. External development + support (FP2)1. Nano satllites5
2. Micro satellites6
3. Small satellites7
4. Large satellites8
3. Independent development + support (JD)1. Nano satellites9
2. Micro satellites10
3. Small satellites11
4. Large satellites12
4. Independent development (DD)1. Nano satellites13
2. Micro satellites14
3. Small satellites15
4. Large satellites16
Table 3. Data analysis of Satellite Technology Ladder (SaTL).
Table 3. Data analysis of Satellite Technology Ladder (SaTL).
TypeCountriesMean SaTLAvg. Years to Transition FP1 to FP2/JDAvg. Years to First DDWeight Class Increase for DD
Type 1Nigeria, Algeria68NANA
Type 2Chile, Thailand, Malaysia, Egypt7.62622.50.25
Type 3Singapore, UAE9.7111162
Type 4Argentina, Turkiye, Iran, Pakistan, South Africa, Peru12.35NA3.171.83
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Fuse, T.; Sapkota, E.; Minato, N.; Antara, R.S.I. Space Development Capacity Building in Emerging Countries: A Technology Ladder Approach to Satellite Systems. Aerospace 2026, 13, 330. https://doi.org/10.3390/aerospace13040330

AMA Style

Fuse T, Sapkota E, Minato N, Antara RSI. Space Development Capacity Building in Emerging Countries: A Technology Ladder Approach to Satellite Systems. Aerospace. 2026; 13(4):330. https://doi.org/10.3390/aerospace13040330

Chicago/Turabian Style

Fuse, Tetsuhito, Eliza Sapkota, Nobuaki Minato, and Raihana Shams Islam Antara. 2026. "Space Development Capacity Building in Emerging Countries: A Technology Ladder Approach to Satellite Systems" Aerospace 13, no. 4: 330. https://doi.org/10.3390/aerospace13040330

APA Style

Fuse, T., Sapkota, E., Minato, N., & Antara, R. S. I. (2026). Space Development Capacity Building in Emerging Countries: A Technology Ladder Approach to Satellite Systems. Aerospace, 13(4), 330. https://doi.org/10.3390/aerospace13040330

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