Entry descent and landing systems for small planetary missions: Parametric comparison of parachutes and inflatable systems for the proposed Vanguard Mars mission-Reference-Cited by-同舟云学术

Entry descent and landing systems for small planetary missions: Parametric comparison of parachutes and inflatable systems for the proposed Vanguard Mars mission

Published:2006-10 Issue:8-11 Volume:59 Page:911-922
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Allouis E.,Ellery A.,Welch C.S.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference12 articles.

1. Mars pathfinder entry, descent, and landing reconstruction;Spencer;Journal of Spacecraft and Rockets,1999

2. J. Stein, C. Standy, Recent Development in Inflatable Airbag Attenuation Systems or Mars Exploration, AAAF-061, Atmospheric Reentry Vehicles and Systems Conference, Arcachon, 2003.

3. W.H. Willcockson, Mars pathfinder heatshield design and flight experience, Journal of Spacecraft and Rockets 36 (3) 374–379.

4. Vanguard, a proposed mission to Mars, mission analysis, and design, KU-VG-DOC-01;Allouis,2003

5. Inflatable reentry and descent technology (IRDT), 15th International Symposium on Spaceflight Dynamics;Wilde,2000

Cited by 7 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Prediction and effect analysis for equilibrium profile of flexible porous canopy fabric;Journal of Industrial Textiles;2022-08

2. DEM-FEM Coupling Analysis of Safe Landing of Reentry Capsule Considering Landing Attitude and Rebound Response;Journal of Aerospace Engineering;2021-07

3. Mars Entry, Descent, and Landing Spacecraft Design to Trajectory Simulation;AIAA Scitech 2021 Forum;2021-01-04

4. Disturbance observer based model predictive control for accurate atmospheric entry of spacecraft;Advances in Space Research;2018-05

5. Development of finite element model for morphing inflatable winglet;Aerotecnica Missili & Spazio;2015-04