Comparative Studies of Conceptual Design and Qualification Procedures for a MARS Probe/Lander. Volume V Subsystem and Technical Analyses. Book 2 - Aeromechanics and Thermal Control Final Report
Comparative Studies of Conceptual Design and Qualification Procedures for a MARS Probe/Lander. Volume V Subsystem and Technical Analyses. Book 2 - Aeromechanics and Thermal Control Final Report
- Neue Suche nach: R. M. Davis
- Neue Suche nach: R. M. Davis
Dokumentinformationen
Comparative Studies of Conceptual Design and Qualification Procedures for a MARS Probe/Lander. Volume V Subsystem and Technical Analyses. Book 2 - Aeromechanics and Thermal Control Final Report
1966
868 pages
Report
Keine Angabe
Englisch
Manned Spacecraft , Atmospheric entry , Conical shell , Mars probe , Spacecraft design , Thermal environment , Aerodynamics , Approach , Atmospheric , Cone , Control , Design , Entry , Environment , Mars , Orbit , Planet , Probe , Shell , Spacecraft , Structure , Thermal , Thermodynamics , Trajectory