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Article

ComputationalAnalysis of a Towed Jumper During Static Line Airborne Operations: A Parametric Study Using Various Airdrop Configurations †

by
Usbaldo Fraire, Jr.
1,‡,
Mehdi Ghoreyshi
2,*,‡,
Adam Jirasek
2,‡,
Keith Bergeron
1,‡ and
Jürgen Seidel
2,*,‡
1
U.S. Army Combat Capabilities Development Command Soldier Center, Natick, MA 01760, USA
2
High Performance Computing Research Center, U.S. Air Force Academy USAF Academy, USAF Academy, CO 80840, USA
*
Authors to whom correspondence should be addressed.
This article is an extended version of the paper entitled “Computational Analysis of a Towed Jumper During Static Line Airborne Operations: A Parametric Study Using Various Airdrop Configurations”, presented at AIAA AVIATION FORUM AND ASCEND 2025, Las Vegas, NV, USA, 29 July–2 August 2024, AIAA Paper 2025–3504.
These authors contributed equally to this work.
Aerospace 2025, 12(10), 897; https://doi.org/10.3390/aerospace12100897
Submission received: 11 July 2025 / Revised: 12 September 2025 / Accepted: 29 September 2025 / Published: 3 October 2025
(This article belongs to the Special Issue Advancing Fluid Dynamics in Aerospace Applications)

Abstract

This study uses the CREATETM-AV/Kestrel simulation software to model a towed jumper scenario using standard aircraft settings to quantify paratrooper stability and risk of contact during static line airborne operations. The focus areas of this study include a review of the technical build-up, which includes aircraft, paratrooper and static line modeling, plus preliminary functional checkouts executed to verify simulation performance. This research and simulation development effort is driven by the need to meet the analysis demands required to support the US Army Personnel Airdrop with static line length studies and the North Atlantic Treaty Organization (NATO) Joint Airdrop Capability Syndicate (JACS) with airdrop interoperability assessments. Each project requires the use of various aircraft types, static line lengths and exit procedures. To help meet this need and establish a baseline proof of concept (POC) simulation, simulation setups were developed for a towed jumper from both the C-130J and C-17 using a 20-ft static line to support US Army Personnel Airdrop efforts. Concurrently, the JACS is requesting analysis to support interoperability testing to help qualify the T-11 parachute from an Airbus A400M Atlas aircraft, operated by NATO nations. Due to the lack of an available A400M geometry, the C-17 was used to demonstrate the POC, and plans to substitute the geometry are in order when it becomes available. The results of a nominal Computational Fluid Dynamics (CFD) simulation run using a C-17 and C-130J will be reviewed with a sample of the output to help characterize performance differences for the aircraft settings selected. The US Army Combat Capabilities Development Command Soldier Center (DEVCOM-SC) Aerial Delivery Division (ADD) has partnered with the US Air Force Academy (USAFA) High Performance Computing Research Center (HPCRC) to enable Modeling and Simulation (M&S) capabilities that support the Warfighter and NATO airdrop interoperability efforts.
Keywords: CFD; airdrop; static line; cable modeling; contact modeling CFD; airdrop; static line; cable modeling; contact modeling

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MDPI and ACS Style

Fraire, U., Jr.; Ghoreyshi, M.; Jirasek, A.; Bergeron, K.; Seidel, J. ComputationalAnalysis of a Towed Jumper During Static Line Airborne Operations: A Parametric Study Using Various Airdrop Configurations. Aerospace 2025, 12, 897. https://doi.org/10.3390/aerospace12100897

AMA Style

Fraire U Jr., Ghoreyshi M, Jirasek A, Bergeron K, Seidel J. ComputationalAnalysis of a Towed Jumper During Static Line Airborne Operations: A Parametric Study Using Various Airdrop Configurations. Aerospace. 2025; 12(10):897. https://doi.org/10.3390/aerospace12100897

Chicago/Turabian Style

Fraire, Usbaldo, Jr., Mehdi Ghoreyshi, Adam Jirasek, Keith Bergeron, and Jürgen Seidel. 2025. "ComputationalAnalysis of a Towed Jumper During Static Line Airborne Operations: A Parametric Study Using Various Airdrop Configurations" Aerospace 12, no. 10: 897. https://doi.org/10.3390/aerospace12100897

APA Style

Fraire, U., Jr., Ghoreyshi, M., Jirasek, A., Bergeron, K., & Seidel, J. (2025). ComputationalAnalysis of a Towed Jumper During Static Line Airborne Operations: A Parametric Study Using Various Airdrop Configurations. Aerospace, 12(10), 897. https://doi.org/10.3390/aerospace12100897

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