Investigation of integrated aerobraking spacecraft and associated technology implications in order to evaluate advantages and disadvantages of this mode; included are parameter and conceptual design studies to define spacecraft weights and their sensitivity to variations in environmental models assumed, crew size, mission profile, propellants, etc, as well as internal packaging arrangements; secondary objective was to analyze requirements for system simulation, testing, and qualification. (15691)
Study of technology requirements for atmosphere braking to orbit about mars and venus
NASA CR
NASA Contractor Reports ; 1 , n 1131
1968
23 pages
Report
English
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Designing of deployment sequence for braking and drift systems in atmosphere of Mars and Venus
British Library Conference Proceedings | 2006
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