Design and Development of the 24-Ft Diam Hybrid Mevlar- 29/Nylon Ribbon Parachute

Author:

Pepper William B.1

Affiliation:

1. Sandia Laboratories, Albuquerque, N. Mex.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 6 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. Designing a Universal Deceleration System for Sounding Rockets Lighter than 100kg by System Engineering Approach;Aeronautics and Aerospace Open Access Journal;2017-07-25

2. Development and testing of subsonic tandem deceleration system;The Aeronautical Journal;2016-10-05

3. 200 kg space payload recovery system;Aerospace Design Conference;1993-02-16

4. Application of Kevlar to parachute system design;Journal of Aircraft;1986-01

5. An experimental study of the performance of clustered parachutes in a low speed wind tunnel;8th Aerodynamic Decelerator and Balloon Technology Conference;1984-04-02

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