Requisite system weights for round trips to Mars from Earth orbit with 7-man crew are presented; analysis of effects of mission duration, radiation environment of space, and use of atmospheric braking.
Study of manned nuclear-rocket missions to Mars
Aerospace Eng
Aerospace Engineering ; 20 , n 7
1961
8 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Online Contents | 1997
Aerothermodynamics of manned Mars missions
NTRS | 1989
|Prospects for Manned Mars Missions
NTRS | 1966
|Aerothermodynamics of manned Mars missions
AIAA | 1989
|