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THE CAPABILITY OF A PROPORATIONAL-TYPE LATERAL CONTROL SYSTEM IN PROVIDING AERDYNAMIC HEADING-ANGLE TRAJECTORY CONTROL DURING REENTRY.

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BookPublisher: Nasa, Washington, D.C. 1964Description: 36.DDC classification: NASA | TN D-2343

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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-2343 (Browse shelf)	Not for loan		TR13038

Total holds: 0

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Previous	NASA TN D-2339 CORRELATION GRAPHS FOR SUPERSONIC FLOW AROUND RIGHT CIRCULAR CONES AT ZERO YAW IN AIR AS A PERFECT GAS	NASA TN D-2340 HEAT-TRANSFER MEASUREMENTS ON A FLAT PLATE AND ATTACHED FINS AT MACH NUMBERS OF 3.51 AND 4.44	NASA TN D-2342 A PRARMETRIC STUDY OF HYPERSONIC FLOW FIELDS ABOUT BLUNT-NOSED CYLINDERS AT ZERO ANGLE OF ATTACK.	NASA TN D-2343 THE CAPABILITY OF A PROPORATIONAL-TYPE LATERAL CONTROL SYSTEM IN PROVIDING AERDYNAMIC HEADING-ANGLE TRAJECTORY CONTROL DURING REENTRY.	NASA TN D-2344 FLOW EVALUATION IN AN ARC-HEATED HYPERSONIC WIND TUNNEL.	NASA TN D-2345 EXPERIMENTAL EVIDENCE OF DEGRADATION EFFECTS IN SHORT SAMPLES OF HARD SUPERCONDUCTORS.	NASA TN D-2346 LOW-SPEED LONGITUDINAL AERODYNAMIC INVESTIGATION OF PARAWINGS AS AUXILILIARY LIFTING DEVICES FOR A SUPERSONIC AIRPLANE CONFIGURATION.	Next

Bound With Nasa Tn D-2340-42,2344-50

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