Author: George R. Smolak
Publisher:
Published: 1962
Total Pages: 100
ISBN-13:
DOWNLOAD EBOOK →Analytical techniques are presented that permit the calculation of heat-transfer rates with various thermal-protection systems for liquid-cryogenic-propellant tanks subjected to on-board, solar, and planetary heat fluxes. The effectiveness of these protection systems in reducing propellant heating is shown both for ideal heat-transfer models and for a simplified hydrogen-oxygen terminal state used for typical Mars missions.
Author: Richard H. Cavicchi
Publisher:
Published: 1962
Total Pages: 48
ISBN-13:
DOWNLOAD EBOOK →Nuclear rocket power levels for unmanned mars vehicles from earth orbit.