Contents include: Unique flexible fibrous material for decelerators; Analysis of an intergrated spacecraft escape system; Unmanned water-to-air recovery system; The effect of space environment on textile materials; Studies of the influence of properities on the landing characteristics of manned spacecraft' Attenuation of deployment and opening forces of certain aerodynamic decelerators; Recovery dynamics for Appollo; Development of the para-sail parachute as a landing system for manned spacecraft; Application of ballistics to precisely control the opening of parachutes, the ultra precision parachute; Attenuation of landing impact for manned spacecraft' Controlled landings with steerable parachutes; Forcible deployment and development of large recovery parachutes for low altitude airdrop of heavy equipment; Flat spin recovery system.
Symposium on Parachute Technology and Evaluation, Proceedings. Volume II
1964
180 pages
Report
No indication
English
Aircraft , Combustion, Engines, & Propellants , Parachutes , Symposia , Parachute fabrics , Escape systems(Aerospace) , Recovery , Air-sea rescues , Lifeboats , Space environmental conditions , Manned spacecraft , Soft landings , Drag parachutes , Gliders , Ballistics , Landing impact , Parachute descents , Spin-recovery parachutes , Apollo , Parasails
Problems of Parachute Technology
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NTIS | 1983
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