Throttleable thrustor system for Mars soft landing, selecting catalytic decomposition engine from system weight and performance studies
Throttleable thruster system design, fabrication and test verification
AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE, 6TH ; 1970 ; SAN DIEGO, CA
01.06.1970
Aufsatz (Konferenz)
Keine Angabe
Englisch
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