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EFFECTS OF FLIGHT CONDITIONS AT BOOSTER SEPRATION ON PLLAYLOAD WEIGHT IN ORBIT.

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BookPublisher: Nasa, Washington, D.C. 1961Description: 45.DDC classification: NASA | TN D-1069

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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-1069 (Browse shelf)	Not for loan		TR15896

Total holds: 0

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Previous	NASA TN D-1066 TRANSITION OF THE LAMINAR BOUNDARY LAYER ON A DELTA WING WITH 74 DEGREE SWEEP IN FREE FLIGHT AT MACH NUMBERS FROM 2.8 TO 5.3	NASA TN D-1067 THE EFFECT OF LATERAL- AND LONGITUDINAL-RANGE CONTROL ON ALLOWABLE ENTRY CONDITIONS FOR A PINT RETURN FROM SPACE.	NASA TN D-1068 SATELLITE ATTITUDE CONTROL UTLIZING THE EARTHS MAGNETIC FIELD.	NASA TN D-1069 EFFECTS OF FLIGHT CONDITIONS AT BOOSTER SEPRATION ON PLLAYLOAD WEIGHT IN ORBIT.	NASA TN D-1070 SKIN STRESSES IN AN INFLATED SPHERE DURING IMPACT.	NASA TN D-1072 HEAT TRANSFER AT THE REATTACHMENT ZONE OF SEPARATED LAMINAR BOUNDARY LAYERS.	NASA TN D-1073 STUDY OF SATELLITE ATTITUDE CONTROL SYSTEM USING INTEGRATION GYROS AS TORQUE SOURCES.	Next

Bound With Nasa Tn D-1061-1068,1070.

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