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THE HYDROGEN-PEROXIDE ROCKET REACTION-CONTROL SYSSTEM FOR THE X-IB RESEARCH AIRPLANE.

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BookPublisher: Nasa, Washington, D.C. 1959Description: 28.DDC classification: NASA | TN D-185

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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-185 (Browse shelf)	Not for loan		TR15745

Total holds: 0

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Previous	NASA TN D-1832 NASA TN [D-1832]	NASA TN D-1838 TRAJECTORY SIMULATION APPLICABLE TO STABILITY AND CONTROL STUDIES OF LARGE MULTI-ENGINE VEHICLES	NASA TN D-184 AN EXPERIMENTAL INVESTIGATION AT A MACH NUMBER OF 4.95 OF FLOW IN THE VICINITY OF A 90 DEGREE INTERIOR CORNER ALINED WITH THE FREE-STREAM VELOCITY.	NASA TN D-185 THE HYDROGEN-PEROXIDE ROCKET REACTION-CONTROL SYSSTEM FOR THE X-IB RESEARCH AIRPLANE.	NASA TN D-1851 - EXPERIMENTAL STUDY OF ONE-AND TWO-COMPONENT LOW TURBULENCE CONFINED COAXIAL FLOWS	NASA TN D-186 A flying-qualities study of a samll ram-jet helicopter.	NASA TN D-187 EXPERIMENTAL INVESTIGATION OF ASPECT-RATOR-1 SUPERCAVITATING HYDROFOILS AT SPEEDS UP TO 185 FEET PER SECOND	Next

Bound With Nasa Tn D-181-184,186-190.

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