An overview of the X-38 prototype crew return vehicle development and test program-Reference-Cited by-同舟云学术

An overview of the X-38 prototype crew return vehicle development and test program

Published:1999-06-08 Issue: Volume: Page:
ISSN:
Container-title:15th Aerodynamic Decelerator Systems Technology Conference
language:
Short-container-title:

Author:

Machin Ricardo¹,Stein Jenny¹,Muratore John¹

Affiliation:

1. NASA, Johnson Space Center, Houston, TX

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1703

Reference8 articles.

1. 'Smith,J.andBennett,T.,evelopmentofthe NASA X-38ParafoilLandingSystem" Paper99-1730tobepresentedat 15tiCEASIAIAA AerodynamicDeceleratorSystemsConference& Seminar,Toulouse,France,June1999.

Cited by 16 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. The Effect of Rigging Angle on Longitudinal Direction Motion of Parafoil-Type Vehicle: Basic Stability Analysis and Wind Tunnel Test;International Journal of Aerospace Engineering;2020-12-07

2. Introductory Chapter: Hypersonic Vehicles - Past, Present, and Future Insights;Hypersonic Vehicles - Past, Present and Future Developments;2019-10-02

3. Numerical Study of Extra-Large Parachute’s Pre-Inflation in Finite Mass Situation;Autex Research Journal;2018-06-01

4. Features of the Upgraded Imaging for Hypersonic Experimental Aeroheating Testing (IHEAT) Software;32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference;2016-06-10

5. Comparative DSSA Study of Payload-Container Dynamics Prior to, During and After Parachute Inflation;19th AIAA Aerodynamic Decelerator Systems Technology Conference and Seminar;2007-05-21