NASA technical note: NASA MEMO 59E
By: Mirels, Harold | Washington: National Aeronautics and Space Administration.
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington , D. C. National Aeronautics and Space Administration 1959Description: 49p.Subject(s): One-dimensional flows
| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA MEMO 59E | Not for loan | 102448 |
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
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