COMBINED EFFECT OF CONTRACTION RATIO AND CHAMBER PRESSURE ON THE PERFORMANCE OF A GASEOUS-HYDROGEN-LIQUID-OXYGEN COMBUSTOR FOR A GIVEN PROPELLANT WEIGHT FLOW AND OXIDANT-FUEL RATIO
By: Hersch,Martin.
Material type:
BookPublisher: Nasa, Washington, D.C. 1961Description: 13.DDC classification: NASA | TN D-129
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-129 (Browse shelf) | Not for loan | TR15637 |
Total holds: 0
Bound With Nasa Tn D-121-128,130
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