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Flight test performance and description of a rocket vehicle for producing low speed artificial meteors.

By: Clarence A Brown.

Contributor(s): Jean C Keating.

Material type: materialTypeLabel

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BookPublisher: DDC classification: NASA | TN D-2270

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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-2270 (Browse shelf)	Not for loan		TR13932

Total holds: 0

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Previous	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	NASA TN D-2273 FREQUENCY RANGES FOR EXISTENCE OF WAVES IN A COLD,COLLISIONLESS HYDROGEN PLASMA	NASA TN D-2274 SURFACE FAILURE OF ALUMINA BALLS DUE TO REPEATED STRESSES APPLIED IN ROLLING CONTACT AT TEMPERATURES TO 2000(DEGRE) F	Next

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