Structural and aerodynamic concepts for centrifugally deployed, variable-geometry atmospheric entry aids are discussed which include means for controlling apex angle of centrifugally stabilized conical flight bodies, concept of isothermal flight, i.e., atmospheric entry at constant surface temperature, and analytical design of optimum rotor-blade structures; materials for flexible rotor construction are classified according to temperature-strength parameter that is characteristic for intended application; application of entry rotor concept to Mars and Earth landing capsule is presented in form of conceptual design configuration. (See also J Spacecraft and Rockets v 2 n 4 July-Aug 1965 p 523-30)
Low-density, autorotating wings for manned re-entry
AIAA -- Tech Papers
Meeting of the AIAA -- Engineering Problems of Manned Interplanetary Exploration ; 1963 Re-entry
1963
29 pages
Conference paper
English
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Low-density, autorotating wings for manned re-entry.
NTRS | 1965
|Low-density, autorotating wings for manned re-entry
AIAA | 1965
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