Rotary Decelerators for Spacecraft: Historical Review and Simulation Results-Reference-Cited by-同舟云学术

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Rotary Decelerators for Spacecraft: Historical Review and Simulation Results

Published:2013-09-10 Issue: Volume: Page:
ISSN:
Container-title:AIAA SPACE 2013 Conference and Exposition
language:
Short-container-title:

Author:

Diaz-Silva Ricardo A.¹,Arellano Daniel²,Sarigulklijn Martinus¹,Sarigul-Klijn Nesrin¹

Affiliation:

1. University of California, Davis

2. Advanced Rotorcraft Technology, Inc.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5361

Reference29 articles.

1. Haig, C. R.,Jr. "The Use ofRotors for theLandingand ReentryBrakingofMannedSpacecraft," IAS Paper No.60-17, Jan.1960.

2. Wernicke R.F. "Preliminary Tests of Model Spacecraft Rotor Landing System," Technical report: Bell Helicopter Space Technology, Brighton, England,May1966.

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1. Autorotation-Based Descent with Trajectory Optimization;Journal of Aircraft;2023-10-24

2. RIPS: Rotor/Impeller Power System;2023 IEEE Aerospace Conference;2023-03-04

3. Design, Analysis, and Testing of a Passively Deployable Autorotative Decelerator;Journal of Aircraft;2022-01

4. Aerodynamic assessment of a rotary entry vehicle for Mars landing: an experimental analysis;Meccanica;2019-04-23

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