Thrust program called perigee propulsion which minimizes gravity loss is analyzed; thrust is applied intermittently in regions of high velocity (near successive perigees); increased energy addition efficiency yields mass ratios approaching those for impulsive velocity change; application and operational aspects of perigee propulsion.
Perigee propulsion for orbital launch of nuclear rockets
NASA -- Tech Report
1962
55 pages
Report
English
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Perigee propulsion for orbital launch of nuclear rockets
TIBKAT | 1962
|PERIGEE PROPULSION FOR ORBITAL LAUNCH OF NUCLEAR ROCKETS
NTRS | 1962
|Perigee propulsion for orbital launch of nuclear rockets
SLUB | 1962
|