The design details are presented of a flight-type heat source reentry vehicle and heat exchanger compatible with the isotope Brayton power conversion system. The reference reentry vehicle and heat exchanger were modified, orbital and superorbital capability was assessed, and a complete set of detail design layout drawings were provided.
Heat source reentry vehicle design study
1971-10-01
Report
Keine Angabe
Englisch
Reentry vehicle nosetip design for minimum total heat transfer
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