Viking Mars hydrazine terminal descent engine thermal design considerations

• 1 January 1977
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
• Vol. 14  (1) , 11-18
• https://doi.org/10.2514/3.27953

Abstract

Keywords

• VIKING MARS
• MARS HYDRAZINE
• THERMAL DESIGN
• TERMINAL DESCENT
• HYDRAZINE TERMINAL
• DESCENT ENGINE
• DESIGN CONSIDERATIONS