The Study of Unidentified Aerial/Aerospace Phenomena Towards Disruptive Propulsion Concepts
A special issue of Aerospace (ISSN 2226-4310). This special issue belongs to the section "Aeronautics".
Deadline for manuscript submissions: 31 January 2027 | Viewed by 486
Special Issue Editors
Interests: hypersonic flows; plasmas; computational fluid dynamics; magnetohydrodynamics; space re-entry systems; space weather; high-performance computing; scientific software design; high-temperature superconductors
Interests: disruptive innovation; technology and capability; multimodal data collection protocols and analytics; knowledge theory; epistemology and research methodology
Special Issue Information
Dear Colleagues,
Unidentified Aerial/Aerospace Phenomena (UAP) have become a topic of growing interest for aerospace scientists, physicists, engineers, defense and the general public at large. This is testified by international research efforts of organizations such as the AIAA UAP Integration and Outreach Committee, Project Hessdalen, SOL Foundation, Scientific Coalition for UAP Studies, Society for UAP Studies and academic projects at Harvard (Galileo Project), Nordic Institute of Theoretical Physics, University of Würzburg (IFEX), Lund University and University of Albany (UAlbany Project X), involving scholars/researchers from different disciplines, particularly engineers and physicists. Such multi-disciplinary research efforts have recently culminated into a number of high-impact scientific publications, de facto establishing the new science of UAPs and opening up new timely opportunities for advancing academic research on this potentially disruptive subject, particularly for aerial/aerospace technologies.
While recent scientific literature has mostly focused on a comprehensive review and detailed analysis for a small representative selection of historical UAP cases for which enough multi-instrumental data were available to be studied, the proposed Special Issue aims to move the discussion further by addressing two main research questions:
- What latest developments in multi-modal/multi-instrumental data collection and analysis allow for better tracking UAPs and characterizing their performance?
- What disruptive physics-based propulsion concepts may (attempt to) explain the reported performance and observables (e.g., hypersonic velocity, absence of sonic boom or heat signature, instantaneous accelerations, trans-medium capability)?
While systematically collecting and analysing data, including with the help of AI-driven algorithms/systems, is essential to better characterise UAPs, the end goal remains to translate the observables into insights/inspiration to build new disruptive technologies providing enhanced performance for aerial/aerospace systems. This Special Issue aims to bridge both of these aspects, combining empirical/technical contributions about detection/tracking and reproducible data analysis of UAPs to better characterize their performance with first-principle theories/models possibly able to reproduce such an observed performance, leading to innovative propulsion systems (e.g., plasma-driven, field-based) that are under current investigation. Such innovative propulsion mechanisms must result from physics-based, hypothesis-driven research with testable prediction/validation pathways, ideally proposing suitable experimental techniques/setups, mathematical/computational models or advanced materials (e.g., high-temperature superconductors, metamaterials) with verifiable properties to enable their development.
Dr. Andrea Lani
Dr. Anders Warell
Gary V. Stephenson
Guest Editors
Manuscript Submission Information
Manuscripts should be submitted online at www.mdpi.com by registering and logging in to this website. Once you are registered, click here to go to the submission form. Manuscripts can be submitted until the deadline. All submissions that pass pre-check are peer-reviewed. Accepted papers will be published continuously in the journal (as soon as accepted) and will be listed together on the special issue website. Research articles, review articles as well as short communications are invited. For planned papers, a title and short abstract (about 250 words) can be sent to the Editorial Office for assessment.
Submitted manuscripts should not have been published previously, nor be under consideration for publication elsewhere (except conference proceedings papers). All manuscripts are thoroughly refereed through a single-blind peer-review process. A guide for authors and other relevant information for submission of manuscripts is available on the Instructions for Authors page. Aerospace is an international peer-reviewed open access monthly journal published by MDPI.
Please visit the Instructions for Authors page before submitting a manuscript. The Article Processing Charge (APC) for publication in this open access journal is 2400 CHF (Swiss Francs). Submitted papers should be well formatted and use good English. Authors may use MDPI's English editing service prior to publication or during author revisions.
Keywords
- unidentified aerial phenomena
- unidentified aerospace phenomena
- hypersonics
- multi-sensor systems
- hyper-spectral cameras
- AI-driven data analysis
- tracking systems
- trans-medium
- electrodynamics
- magnetohydrodynamics
- field propulsion
- quantum gravity
Benefits of Publishing in a Special Issue
- Ease of navigation: Grouping papers by topic helps scholars navigate broad scope journals more efficiently.
- Greater discoverability: Special Issues support the reach and impact of scientific research. Articles in Special Issues are more discoverable and cited more frequently.
- Expansion of research network: Special Issues facilitate connections among authors, fostering scientific collaborations.
- External promotion: Articles in Special Issues are often promoted through the journal's social media, increasing their visibility.
- Reprint: MDPI Books provides the opportunity to republish successful Special Issues in book format, both online and in print.
Further information on MDPI's Special Issue policies can be found here.

