PROPELLANT VAPORIZATION AS A CRITERION FOR ROCKET-ENGINE DESIGN; EXPERIMENTAL PERFORMANCE, VAPORIZATION, AND HEAT-TRANSFER RATES WITH VARIOUS PROPELLANT COMBINATIONS [NASA MEMO 12-29-58E]
Material type:
TextLanguage: English Series: National Aeronautics and Space Administration | NASA Technical NotePublication details: National Aeronautics and Space Administration 1959 Washington, D.C.Description: 31p
| Item type | Current library | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds | |
|---|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA MEMO 12-28-58E-12-29-58E | Not for loan | TR014070 |
Total holds: 0
Bound With Nasa Memo 12-8-58E-12-29-58E
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