EVALUATION OF INJECTOR PRINCIPLES IN A 2400-POUND-THRUST ROCKET ENGINE USINJG LIQUID OXYGEN AND LIQUID AMMONIA
By: Hendricks,Robert C,Ehlers,Robert C.
Contributor(s): Graham,Robert W.
Material type:
BookPublisher: Nasa, Washington, D.C. 1959Description: 33.DDC classification: NASA | MEMO 12-11-58E
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA MEMO 12-11-58E (Browse shelf) | Not for loan Untraceable | TR14064 |
Total holds: 0
Bound With Nasa Memo 12-8-58e-12-10-58e, 12-13-58e-12-29-58e Lack No.12-9-58e, 12-12-58e, 12-14-58e-12-20-58e, 12-25-58e-12-28-58e.
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