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EARTH OBLATENESS AND RELATIVE SUN MOTION CONSIDERATIONS IN THE DETERMINATION OF AN IDEAL ORBIT FOR THE NIMBUS METEROLOGICAL SATELLITE

By: Bandeen,William R.

Series: NASA Technical Note. D-1045.Publisher: NASA, Washington, D.C. 1961Description: 10p.Subject(s): Aerodynamics

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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-1045	Not for loan		TR8631

Total holds: 0

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Previous	NASA Technical Note: FLIGHT TESTS OF DIRECT LIFT CONTROL SYSTEM DURING APPROACH AND LANDING	NASA Technical Note: AERODYNAMIC CHARACTERISTICS OF A PARASOL-WING-BODY COMBINATION UTILIZING FAVORABLE LIFT INTERFERENCE AT MACH NUMBERS FROM 3.00 TO 4.63	NASA TN [D-1044]	EARTH OBLATENESS AND RELATIVE SUN MOTION CONSIDERATIONS IN THE DETERMINATION OF AN IDEAL ORBIT FOR THE NIMBUS METEROLOGICAL SATELLITE	EXPERIMENTAL INVESTIGATION OF AN AIR-COOLED TURBINE OPERATING IN A TURBOJET ENGINE AT TURBINE INLET TEMPERATURES UP TO 2500(DEGREE)	NASA TN [D-1047]	ANNULAR INTERNAL-EXTERNAL-EXPANSION ROCKET NOZZLES FOR LARGE BOOSTER APPLICATIONS	Next

Technical Note D-1041-50
Bound Vol. No.65506; Contents: TR8629-36

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