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FEASIBILITY, PARAMETRIC DESIGN, AND COMPARATIVE ANALYSIS OF AN UNGUIDED SOLID FUEL ROCKET VEHICLE WITH SOLAR ORBIT, EARTH PROBE, AND RE-ENTRY MISSION CAPABILITIES.

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BookPublisher: Nasa, Washington, D.C. 1967Description: 146.DDC classification: NASA | CR-753

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA CR-753 (Browse shelf)	Not for loan		TR11912

Total holds: 0

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Previous	NASA CR-749 - EXPERIMENTAL STUDY OF SUPERLAMINAR FLOW BETWEEN NONCONCENTRIC ROTATING CYLINDERS	NASA CR-750 - GEOMETRIC THEORY OF OPTIMUM DISORBIT PROBLEMS	NASA CR-752 A PROGRAM OF HIGH ANGULAR RESOLUTION STUDIES OF CELESTIAL X-RAY SOURCES.	NASA CR-753 FEASIBILITY, PARAMETRIC DESIGN, AND COMPARATIVE ANALYSIS OF AN UNGUIDED SOLID FUEL ROCKET VEHICLE WITH SOLAR ORBIT, EARTH PROBE, AND RE-ENTRY MISSION CAPABILITIES.	NASA CR-754 AN EXPERIMENTAL STUDY OF PRESSURE DISTRIBUTION CURVES APPLICABLE TO PNEUMATIC TIRES.	NASA CR-755 APPLICATIONS OF ARTIFICIAL INTELLIGENCE TECHNIQUES TO A SPACECRAFT CONTROL PROBLEM.	NASA CR-757 ANALYTICAL STUDY OF IMPACT EFFECTS AS APPLIED TO THE METEOROID HAZARD	Next

Bound With Nasa Cr-751-52, 754-55

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