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STUDY OF DIRECT-RETURN RENDZVOUS TRAJECTORIES USING CONSTANT-THURST ENGINES AND RENDEZVOUS OR MANEUERING THRUSTERS.

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BookPublisher: Nasa, Washington, D.C. 1965Description: 21.DDC classification: NASA | TN D-3019

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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 TN D-3019 (Browse shelf)	Not for loan		TR16098

Total holds: 0

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Previous	NASA TN D-3017 PRESSURE AND CONVECTIVE HEAT-TRANSFER MEASUREMENTS IN A SHOCK TUNNEL USING SEVERAL TEST GASES.	NASA TN D-3017 PRESSURE AND CONVECTIVE HEAT-TRANSFER MEASUREMENTS IN A SHOCK TUNNEL USING SEVERAL TEST GASES.	NASA TN D-3018 HYPERVELOCITY IMPACT CHARACTERISTICS IN BERYLLIUM AND GRAPHITE PLATES AND TUBES.	NASA TN D-3019 STUDY OF DIRECT-RETURN RENDZVOUS TRAJECTORIES USING CONSTANT-THURST ENGINES AND RENDEZVOUS OR MANEUERING THRUSTERS.	NASA TN D-3020 EQUATIO OF STATE OF MATTER AT SUPERNULEAR DENSITY.	NASA TN D-3032 - EXPERIMENTAL STUDY OF TRANSIENT EFFECTS IN DIELECTRIC MATERIALS CAUSED BY ELECTRON IRRADIATION	NASA TN D-3033 - MASS SPECTROMETRIC ANALYSIS OF DC 704 DIFFUSION-PUMP OIL FRAGMENTATION	Next

Bound With Nasa Tn D-3011-3018,3020.

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