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Equations of motion and design criteria for the despin of a vehicle by the radial release of weights and cables of finite mass[NASA TN D-1012]

By: Eide,Donald G.

Contributor(s): Vaughan,Chester A.

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BookSeries: National Aeronaitics and Space Adminstration ; NASA Technical Note. Publisher: Wahington.D. C. National Aeronaitics and Space Adminstration 1962Description: 49p.Subject(s): Despin of a vehicle

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	COMPACT STORAGE (BASEMENT)	NASA TN D 1011-1020 (Browse shelf)	Not for loan		TR010369

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser

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Previous	NASA TN 4083 Investigation over moving ground plane of a transport airplane model using blowing over flaps for boundary-layer control. [NASA TN D-4083]	NASA TN CR-1506 RADIO ASTRONOMICAL STUDIES WITH 1500-METER DIAMETER LOW-FREQUENCY TELESCOPE.	NASA TN D - 690 Aerodynamic loads at mach numbers from 0.70 to 2.22 on airplane model having a wing and canard of triangular plan form and either single or twin vertical tails [NASA TN D-690]	NASA TN D 1011-1020 Equations of motion and design criteria for the despin of a vehicle by the radial release of weights and cables of finite mass[NASA TN D-1012]	NASA TN D- 1481 Aerodynamic characteristics of four-duct tandem VTOL-aircraft configurations [NASA TN D- 1481]	NASA TN D- 1751 Electron density distribution in the upper F- region [NASA TN D- 1751-- TN D-1760]	NASA TN D 1821-1830 Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles	Next

Bound vol. contains NASA TN D 1011- 1020

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