Design and development of a heavy duty 76-ft ribbon parachute
Author:
Affiliation:
1. SANDIA CORP., SANDIA LAB., AEROTHERMODYNAMICS DEPT., ALBUQUERQUE, N. MEX.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1968-930
Reference1 articles.
Cited by 4 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. STUDY OF MINIMAL EFFECTIVE REEFING RATIO BASED ON AN EMPIRICAL FORMULA AND FLUID-STRUCTURE-INTERACTION METHOD;Aviation;2018-12-07
2. A coupling apparent mass for parachute inflation equations;10th Aerodynamic Decelerator Conference;1989-04-18
3. Prediction of the Drag Coefficient of a 20' Conical Ribbon Parachute;Journal of Spacecraft and Rockets;1977-03
4. Drag coefficient of 20-degree conical ribbon parachute;5th Aerodynamic Deceleration Systems Conference;1975-08-16
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