Mirels, Harold
NASA technical note: NASA MEMO 59E
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.- Washington , D. C.: National Aeronautics and Space Administration, 1959
.- 49p.
.- ( National Aeronautics and Space Administration NASA Technical Note
NASA MEMO 59E:Source distribution method for unsteady one dimensional flows with small mass momentum and heat addition and small area variation by Harold Mirels 49p NASA MEMO 59E: Analytical investigation of the effect of turnbopump design on gross weight chatectristics of a hydrogen propelled nuclear rocket by Harold E. Rohlik 37p NASA MEMO 59E: Experimental altitude performance of jp-4 fuel and liquid oxygen rocket engine with an area ratio of 48 by Anthony Fortini 27p NASA MEMO 59E: Performance characteristics of flush and shielded auxiliary exits at mach numbers of 1.5 to 2.0 by Kaleel L. Abdalla 21p NASA MEMO 59E: Human tolerance to rapidly applied accelerations a summary of the literature by A. Martin Eiband 91p NASA MEMO 59E: Theoretical performance of liquid oxygen as a rocket propellant by Sanford Gordon 137p NASA MEMO 59E: Effect of ozone addition on combustion efficiency of hydrogen liquid oxygen propellant in small rockets by Riley O. Miller 17p
Subject Headings:
One-dimensional flows;
Copy Details:
Acc. No.: 102448 , Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA MEMO 59E
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