NASA Technical Note: Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines
By: Salmi, Reino J.
Contributor(s): Wanhainen, John P | Hannum, Ned P.
Material type:
BookSeries: NASA Technical Note ; National Aeronautics and Space Administration. Publisher: Washington, D.C. NASA 1968Description: 27p.Subject(s): Coaxial Injectors -- Oxygen-Hydrogen Rocket Engine
| 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 TN D-4851 | Not for loan | 101116 |
Total holds: 0
Bound Volume No.101116 Contents TR 7622-7630
Technical Note D-4851-4860
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