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A FIVE-STAGE SOLID-FUEL SOUNDING-ROCKET SYSTEM

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BookPublisher: Nasa, Washington, D.C. 1959Description: 22.DDC classification: NASA | MEMO 3-6-59L

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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 MEMO 3-6-59L (Browse shelf)	Not for loan		TR7391

Total holds: 0

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Previous	NASA MEMO 3-3-59L WIND-TUNNEL INVESTIGATION OF THE EFFECT OF ANGLE OF ATTACK AND FLAPPING-HINGE OFFSET ON PERIODIC BENDING MOMENTS AND FLAPPING OF A SMALL ROTOR	NASA MEMO 3-4-59L THE SHOCK-WAVE NOISE PROBLEM OF SUPERSONIC AIRCRAFT IN STEADY FLIGHT	NASA MEMO 3-5-59L NOISE PROBLEMS ASSOCIATED WITH GROUND OPERATIONS OF JET AIRCRAFT	NASA MEMO 3-6-59L A FIVE-STAGE SOLID-FUEL SOUNDING-ROCKET SYSTEM	NASA MEMO 3-7-59L INFLUANCE OF LARGE POSITIVE DIHEDRAL ON HEAT TRANSFER TO LEADING EDGES OF HIGHLY SWEPT WINGS AT VERY HIGH MACH NUMBERS	NASA MEMO 3-8-59L WIND-TUNNEL INVESTIGATION OF A SMALL - SCALE SWEPTBACK-WING JET-TRANSPORT MODEL EQUIPPED WITH AN EXTERNAL-FLOW JET-AUGMENTED DOUBLE SLOTTED FLAP	NASA MEMO 4-11-59L - LOW-SPEED STATIC STABILITY AND CONTROL CHARACTERISTICS OF A MODEL OF A RIGHT TRIANGULAR PYRAMID REENTRY CONFIGURATION	Next

Bound With Tr007387, Tr007392-98

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