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Abort separation study of a shuttle orbiter and external tank at hypersonic speeds [NASA TM X-3212]

By: Bernot, Peter T.

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BookSeries: National Aeronautics and Space Administration [NASA]. Publisher: Washington, D.C. National Aeronautics and Space Administration [NASA] 1975Description: 47p.DDC classification: NASA | TM X-3212

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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 TM X-3212 (Browse shelf)	Not for loan		TR002697

Total holds: 0

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

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Previous	NASA SUMM-37-60 FLIGHT PROJECTS	NASA TM - 84584 High-Angle-of-Attack stability characteristics of a three-surface fighter configuration [NASA TM - 84584]	NASA TM X-3191 Aerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade [NASA TM X-3191]	NASA TM X-3212 Abort separation study of a shuttle orbiter and external tank at hypersonic speeds [NASA TM X-3212]	NASA TM X-73434 Preliminary scaling laws for plasma current, ion kinetic temperature, and plasma number density in the NASA lewis bumpy torus plasma	NASA TM X-952 A TABULATION OF HELICOPTER ROTOR-BLADE DIFFEENTIONAL PRESSURE,STRESSES,AND MOTIONS AS MEASURED IN FLIGHT.	NASA TM-75237 Comparison of aerodynamic coefficients obtained from theoretical calculations wind tunnel tests and flight tests data reduction for the alpha jet aircraft	Next

Bound with NASA TM X-3212 to 3219 (TR002697 to TR002703); Lack no. NASA TM X-3217

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