000			01707nam a22002897a 4500
003			OSt
005			20220823152931.0
008			220704b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
100			_aMirels, Harold
110			_aWashington: National Aeronautics and Space Administration
245			_aNASA technical note: NASA MEMO 59E
260			_aWashington , D. C. _bNational Aeronautics and Space Administration _c1959
300			_a49p
440			_aNational Aeronautics and Space Administration
440			_aNASA Technical Note
500			_aNASA 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
500			_aNASA 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
500			_aNASA MEMO 59E: Experimental altitude performance of jp-4 fuel and liquid oxygen rocket engine with an area ratio of 48 by Anthony Fortini 27p
500			_aNASA MEMO 59E: Performance characteristics of flush and shielded auxiliary exits at mach numbers of 1.5 to 2.0 by Kaleel L. Abdalla 21p
500			_aNASA MEMO 59E: Human tolerance to rapidly applied accelerations a summary of the literature by A. Martin Eiband 91p
500			_aNASA MEMO 59E: Theoretical performance of liquid oxygen as a rocket propellant by Sanford Gordon 137p
500			_aNASA MEMO 59E: Effect of ozone addition on combustion efficiency of hydrogen liquid oxygen propellant in small rockets by Riley O. Miller 17p
650			_aOne-dimensional flows
942			_cTR
999			_c565775 _d565775