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ANALYSIS OF THE EFFECT OF ALTIMETER-SYSTEM ACCURACY ON COLLISION PROBABILITY.

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BookPublisher: Nasa, Washington, D.C. 1963Description: 9.DDC classification: NASA | TN D-1627

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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-1627 (Browse shelf)	Not for loan		TR14292

Total holds: 0

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Previous	NASA TN D-1624 INVESTIGATION OF THE SKID-ROCKET LANDING CHRACTERISTICS OF SPACERAFT MODELS.	NASA TN D-1625 THEORITICAL STABILITY ANALYSIS OF SKID-ROCKET LANDINGS OF SPACE VEHICLES.	NASA TN D-1626 EXPERIMENTAL PRESSURES AND TURBULENT HEAT TRANSFER COEFFICIENTS ASSOCIATED EITH SINUSODIAL	NASA TN D-1627 ANALYSIS OF THE EFFECT OF ALTIMETER-SYSTEM ACCURACY ON COLLISION PROBABILITY.	NASA TN D-1630 OFF-DESIGN AERODYNAMIC CHRACTERISTICS AT MACH NUMBERS 1.61 AND 2.20 OF A SERIES OF HIGHLY SWEPT ARROW WINGS DESIGNED FOR MACH NUMBER 2.0 EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER.	NASA TN D-1632 AN EXTENSION OF ESTIMATED HYPERSONIC FLOW PARAMETERS FOR HELIUM AS A REAL GAS	NASA TN D-1633 INVESTIGATION OF BUFFET PRESSURES ON MODELS OF LARGE MANNED LAUNCH VEHICLE CONFIGURATIONS	Next

Bound With Nasa Tn D-1621-1626,1628-1629.Lack No-1628.

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