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SATELITE ATITUDE CONTROL USING A COMBINATION OF INERTIA WHEELS AND A BAR MAGNET

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BookPublisher: Nasa, Washington, D.C. 1960Description: 42.DDC classification: NASA | TN D-626

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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-626 (Browse shelf)	Not for loan		TR12352

Total holds: 0

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Previous	NASA TN D-6257 ANALOG ANALYSIS OF THE HEAVE RESPONSE AND CONTROL OF A PLENUM-TUPE AIR-CUSHION VEHICLE	NASA TN D-6258 A DIFFERENTIAL CORRECTION TECHNIQUE FOR DETERMINING PHYSICAL PROPERTIES OF THE MARTIAN ATMOSPHERE BY USE OF SOLAR OCCULTATION AS SEEN FROM AN ARTIFICIAL SATELLITE	NASA TN D-6259 METAL STRUCTURES WITH PARALLEL PORES OF UNIFORM SIZE	NASA TN D-626 SATELITE ATITUDE CONTROL USING A COMBINATION OF INERTIA WHEELS AND A BAR MAGNET	NASA TN D-6261 PLATE TECTONICS IN THE RED SEA REGION AS INFERRED FROM SPACE PHOTOGRAPHY	NASA TN D-6262 LINEARIZED THEORY OF STAGNATION REGION SKIN FRICTION AND MASS TRANSFER AT HYPERSONIC SPEEDS	NASA TN D-6263 LIFT AND DRAG CHARACTERISTICS OF THE HL-10 LIFTING BODY DURING SUBSONIC GLIDING FLIGHT	Next

Bound With Nasa Tn D-621-625 & 627-630

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