Mars entry, descent, and landing instrumentation 2 trajectory, aerodynamics, and atmosphere reconstruction

CD Karlgaard, M Schoenenberger, S Dutta… - Journal of Spacecraft …, 2023 - arc.aiaa.org
On February 18th, 2021, the Mars 2020 entry system successfully delivered the
Perseverance rover to the surface of Mars at Jezero Crater. The entry capsule carried a set …

Adaptable deployable entry and placement technology sounding rocket one modeling and reconstruction

S Dutta, CD Karlgaard, AM Korzun, JS Green… - Journal of Spacecraft …, 2022 - arc.aiaa.org
Sounding Rocket One (SR-1), the first flight test of the Adaptable Deployable Entry and
Placement Technology (ADEPT), was performed on September 12, 2018. ADEPT is a …

Use of Forecast Atmospheric Data for Earth Entry, Descent, and Landing Missions

S Dutta - Journal of Spacecraft and Rockets, 2024 - arc.aiaa.org
FLIGHT dynamics simulations for entry, descent, and landing (EDL) use atmospheric models
that simulate environments based on historical data. Examples of some of the most common …

Mars InSight entry, descent, and landing trajectory and atmosphere reconstruction

CD Karlgaard, AM Korzun… - Journal of Spacecraft …, 2021 - arc.aiaa.org
The InSight mission landed on the surface of Mars on 26 November 2018. The InSight
system performance met all design requirements, although several performance metrics fell …

Flight Mechanics Analysis of Low-Earth Orbit Flight Test of an Inflatable Decelerator

R Deshmukh, S Dutta, A Bowes… - AIAA SCITECH 2024 …, 2024 - arc.aiaa.org
The Low-Earth Orbit Flight Test of an Inflatable Decelerator (LOFTID) successfully
demonstrated the capability of an inflatable aeroshell. Prior to launch, flight mechanics …

Dragonfly Mission Entry and Descent Modeling and Simulation Overview

AR Pensado, RG Winski, JW Williams… - AIAA SCITECH 2025 …, 2025 - arc.aiaa.org
Dragonfly is a New Frontiers Program mission, led by The Johns Hopkins Applied Physics
Laboratory, that will deliver a rotorcraft lander to Saturn's moon, Titan. The focus of this work …

Advanced Supersonic Parachute Inflation Research Experiment-2 (ASPIRE2) Parachute Modeling and Flight Mechanics Performance

E Roelke, JS Green, S Dutta - AIAA SCITECH 2025 Forum, 2025 - arc.aiaa.org
The Advanced Supersonic Parachute Inflation Research Experiment-2 (ASPIRE2) program
is designed to test and qualify the supersonic parachute for the Mars entry, descent, and …

[HTML][HTML] 火星探测热防护系统传感测量技术进展与启示

宋思琪, 张金刚, 杨强, 易法军, 孟松鹤 - 空气动力学学报, 2024 - pubs.cstam.org.cn
当前对于火星进入, 下降与着陆过程(entry, descent and landing, EDL) 气动环境认知不足,
任务风险高. 在EDL 系统上搭载传感仪器进行飞行数据测量, 重建火星大气和气动热环境 …

[HTML][HTML] Analysis and verification of aerodynamic characteristics of Tianwen-1 mars parachute

M Huang, W Wang, J Li - Space: Science & Technology, 2022 - spj.science.org
The Mars parachute flight environment is supersonic, low-density, and low dynamic
pressures. To ensure the operating performance and reliability, the design optimization and …

Fluid-Structure Interaction Simulations of the ASPIRE SR03 Supersonic Parachute Flight Test

F Cadieux, JB Angel, MF Barad, CC Kiris - AIAA SCITECH 2023 Forum, 2023 - arc.aiaa.org
View Video Presentation: https://doi. org/10.2514/6.2023-1336. vid Research into parachute
performance continues to be a source of significant investment from the National …