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CHARACTERISTICS OF A CONTINUOUS-FLOW INDUCTION PLASMA ACCELERATOR.

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BookPublisher: Nasa, Washington, D.C. Description: 27.DDC classification: NASA | TR R-219

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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 TR R-219 (Browse shelf)	Not for loan		TR11758

Total holds: 0

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Previous	NASA TR R-216 NUCLEATE AND FILM BOILING IN REDUCED GRAVITY FROM HORIZONTAL AND VERTICAL WIRES.	NASA TR R-217 LIOUVILLE'S EQUATION AND THE N-BODY PROBLEM.	NASA TR R-218 POLARIZATION OF PROTONS FROM (D,P) REACTIONS AT 21 MEV.	NASA TR R-219 CHARACTERISTICS OF A CONTINUOUS-FLOW INDUCTION PLASMA ACCELERATOR.	NASA TR R-220 ANALYSIS OF HEAT-TRANSFER EFFECTS IN ROCKET NOZZLES OPERATING WITH VERY HIGH-TEMPERATURE HYDROGEN.	NASA TR R-222 EQUATIONS FOR ISENTROPIC AND PLANE SHOCK FLOWS OF MIXTURES OF UNDISSOCIATED PLANETARY GASES	NASA TR R-223 A PERFECT-GAS ANALYSIS OF THE EXPANSION TUNNEL, A MODIFICATION TO THE EXPANSION TUBE	Next

Bound With Nasa Tr R-211-18, 220

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