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PRELIMINARY ANALYSIS OF A SIMULATED METEOR REENTRY AT 9.8 KILOMETERS PER SECOND.

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BookPublisher: Nasa, Washington, D.C. 1964Description: 22.DDC classification: NASA | TN D-2268

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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-2268 (Browse shelf)	Not for loan		TR13930

Total holds: 0

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Previous	NASA TN D-2265 FLIGHT EVALUATION OF WIDE-ANGLE, OVERLAPPING MONOCULARS FOR PROVIDING PILOT'S FIELD OF VISION.	NASA TN D-2266 REVIEW OF SOME RECENT RESEARCH ON NOISE AND STRUCTURAL VIBRATION.	NASA TN D-2267 HYDROSTATIC STABILITY OF THE LIQUID-VAPOR INTERFACE IN A GRAVATIONAL FIELDS.	NASA TN D-2268 PRELIMINARY ANALYSIS OF A SIMULATED METEOR REENTRY AT 9.8 KILOMETERS PER SECOND.	NASA TN D-2269 WIDE RANGE PHASE DETECROR.	NASA TN D-2270 Flight test performance and description of a rocket vehicle for producing low speed artificial meteors.	NASA TN D-2272 HALL EFFECT DEVICES AS MAGNETOMETERS IN CRYOGENIC APPLICATIONS	Next

Bound With Nasa Tn D-2261-2267,2269-2270.

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