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PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL.

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BookPublisher: Nasa, Washington, D.C. 1969Description: 38.DDC classification: NASA | TN D-5597

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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-5597 (Browse shelf)	Not for loan		TR12671

Total holds: 0

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Previous	NASA TN D-5593 THE ROLE OE STAGED SPACE PROPULSION SYSTEMS IN INTERPLANETARY MISSIONS.	NASA TN D-5595 AUTOMATIC ANALOG COMPUTER SCALING USING DIGITAL OPTIMIZATION TECHNIQUES.	NASA TN D-5596 OBLIQUE ECHOES FROM LARGE-SCALE HORIZONTAL GRADIENTS OBSERVED BY ALOUETTE-2 TOPSIDE SOUNDER.	NASA TN D-5597 PERFORMANCE OF A 48-MODULE SWIRL-CAN TURBOJET COMBUSTOR SEGMENT AT HIGH TEMPERATURES USING ASTM-A1 FUEL.	NASA TN D-5598 A PROPOSED METHOD FOR REGENERATION OF NEUTRON PRODUCING TARGETS, WITHIN AN ACCELERATOR, BY ION SPUTTERING TECHNIQUES.	NASA TN D-5599 DYNAMICS OF TWO SLOWLY ROTATING POINT-MASS VEHICLES CONNECTED BY A MASSLESS TETHER AND IN A CIRCULAR ORBIT.	NASA TN D-5601 AN ANALYSIS OF VGH DATA COLLECTED FROM ONE TYPE OF FOUR-ENGINE TURBOJET TRANSPORT AIRPLANE	Next

Bound With Nasa Tn D-5590-96, 5598-99 Lack No.5594

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