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ANALYTIC CALCULATION OF LAUNCH VEHICLE RESPONSE TO WINDS AND CALCULATION OF OPTIMAL BIASED PITCH PROGRAMS.

Series: NASA Technical Note. Publisher: NASA, Washington, D.C. 1970Description: 39p.Subject(s): Aerospace

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Item type	Current location	Collection	Call number	Vol info	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)		NASA TN D-5823	Not for loan		TR11717

Total holds: 0

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Previous	Report of Investegations 7656	Geometric properties of a modified whriling-membrane solar-energy concentrator [NASA TN D-5859]	Evaluation of a vtol flight-director concept during constant-speed instrument approaches [NASA TN D-5860]	ANALYTIC CALCULATION OF LAUNCH VEHICLE RESPONSE TO WINDS AND CALCULATION OF OPTIMAL BIASED PITCH PROGRAMS.	FILMENTARY CRYSTAL GROWTH ASSOCIATED WITH HYPER VELOCITY MICROPRATICLE IMPACT CRATERS	METHOD FOR CALCULATING ROCKET ENGINE STRUCTURAL LOADS.	INVESTIGATION OF A DIGITAL SIMULATION OF THE XB-70 INLET AND ITS APPLICATION TO FLIGHT-EXPERIENCED FREE- STREAM DISTURBANCE AT MACH NUMBERS OF 2.4 TO 2.6	Next

Technical Reports D-5821-30
Bound Vol. No.101201; Contents: TR11715-24

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