The Concept of a Rocket Engine Using CO2/Metal Propellant for Mars Sample Return Missions

Details The Concept of a Rocket Engine Using CO2/Metal Propellant for Mars Sample Return Missions The Concept of a Rocket Engine Using CO2/Metal Propellant for Mars Sample Return Missions

Dec 2000

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2000esasp.465..219g&link_type=gif

Spacecraft Propulsion, Third International Conference held 10-13 October, 2000 at Cannes, France. Edited by R.A. Harris. Europ

Physics

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