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A THREE-STAGES SOLID-FUEL SOUNDING ROCKET SYSTEM SUITABLE FOR RESEARCH AT ALTITUDES NEAR 200 NAUTICAL MILES.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 25.DDC classification: NASA | TN D-219

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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-219 (Browse shelf)	Not for loan		TR13110

Total holds: 0

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Previous	NASA TN D-2188 RADIATION FROM SLOTTED-CYLINDER ANTENNAS IN A REENTRY PLASMA ENVIRONMENT	NASA TN D-2188 SOME EXPERIMENTAL RESULTS FOR A DOPPLER TRACKING METHOD USING A SIMPLE CW BEACON	NASA TN D-2189 DESCRIPTION OF VEHICLE SYSTEM AND FLIGHT TESTS OF NIN TRAILBLAZER I REENTRY PHYSICS RESEARCH VEHICLES	NASA TN D-219 A THREE-STAGES SOLID-FUEL SOUNDING ROCKET SYSTEM SUITABLE FOR RESEARCH AT ALTITUDES NEAR 200 NAUTICAL MILES.	NASA TN D-2190 SUPERSONIC LONGITUDINAL STABILITY CHARACTERISTICS OF THE TWO FINAL STAGES OF A FOUR-STAGE LAUNCH VEHICLE	NASA TN D-2192 - FLUTTER OF CURVED AND FLAT SANDWICH PANELS SUBJECTED TO SUPERSONIC FLOW	NASA TN D-2193 - FFECTS OF LAMINAR-BOUNDARY -LAYER DISPLACEMENT ON A HEMISPHERE IN HELIUM FLOW	Next

Bound With Nasa Tn D-211-218,220

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