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CONCEPTUAL STUDY OF ROCKET-SCRAMJET HYBRID ENGINES IN A LIFTING REUSABLE SECOND STAGE.

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BookPublisher: Nasa, Washington, D.C. 1969Description: 52.DDC classification: NASA | TN D-5218

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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-5218 (Browse shelf)	Not for loan		TR15283

Total holds: 0

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Previous	NASA TN D-5215 A NEW MOMENTUM-INTEGRAL METHOD FOR TREATING MAGNETOHYDRODYNAMIC AND SIMPLE HYDRODYNAMIC ENTRANCE FLOWS.	NASA TN D-5216 STUDY OF THE (D,T) REACTION ON SCANDIUM-45 AT 41 MEV.	NASA TN D-5217 ANALYSIS OF ELECTRON ANALOG SIMULATION OF ION CONTAINMENT IN MAGNETIC FIELDS.	NASA TN D-5218 CONCEPTUAL STUDY OF ROCKET-SCRAMJET HYBRID ENGINES IN A LIFTING REUSABLE SECOND STAGE.	NASA TN D-5219 STATIC LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF SOME SUPERSONIC DECELERATOR MODELS AT MACH NUMBERS OF 2.30 AND 4.63.	NASA TN D-5220 AN ANALYSIS OF TERRAIN BIAS ERROR IN PLANETARY RADAR ALTIMETERS.	NASA TN D-5221 THE EQUIPMENTIAL SPACE-SUIT DESIGN CONCEPT AND ITS APPLICATION TO A SPACE-SUIT ELBOW JOINT.	Next

Bound With Nasa Tn D-5211-5217,5219-5230.

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