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Flight measurement of stability and control derivatives of the x-15 research air[lane to a mach number of 6.02 and an angle of attack of 25 degree. [NASA TN D-2532]

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BookSeries: National Aeronautics and Space Administration (NASA). Publisher: Washington, D.C. Nasa, 1964Description: 47p.Subject(s): derivatives

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NASA technical report

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D-2532 (Browse shelf)	Not for loan		TR15991

Total holds: 0

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Previous	NASA TN D-2500 - RENDEZVOUS CAPABILITY OF HORIZONTAL-TAKE-OFF LAUNCH VEHICLE WITH AIR-BREATHING PROPULSION	NASA TN D-2501 Surface pressure and turbulent airflow in transverse rectangular notches [NASA TN D-2501--TN D-2510]	NASA TN D-2531 A technique for visuval detection of distant object in space by use of optical filtering. [NASA TN D-2531]	NASA TN D-2532 Flight measurement of stability and control derivatives of the x-15 research air[lane to a mach number of 6.02 and an angle of attack of 25 degree. [NASA TN D-2532]	NASA TN D-2533 Vibration and stability analysis of compressed rocke vehicles.	NASA TN D-2534 A Radiation climatology in the visible and infrared from the tiros meteorogical satellites [NASA TN D-2534]	NASA TN D-2535 Conversion of a spacecraft designed for manned space flight to a recoverable orbiting astronomical observatory. NASA TN D-2535]	Next

NASA technical report

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