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]
By: Clark, Bruce J.
Material type: BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D.C. National Aeronautics and Space Administration 1959Description: 31p.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 12-28-58E-12-29-58E | Not for loan | TR014070 |
Total holds: 0
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Bound With Nasa Memo 12-8-58E-12-29-58E
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