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PERFORMANCE AND SOME DESIGN ASPECTS OF THE FOUR-STAGE SOLID-PROPELLANT ROCKET VEHICLE USED IN THE RAM A1 FLIGHT TEST

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BookPublisher: Nasa, Washington, D.C. 1963Description: 49.DDC classification: NASA | TN D-1611

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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-1611 (Browse shelf)	Not for loan		65569

Total holds: 0

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Previous	NASA TN D-1606 AERODYNAMIC CHRACTERISTICS AT A MACH NUMBER OF 6.77 OF A 9 DEGREE CONE CONFIGURATION, WITH AND WITHOUT SPHERICAL AFTERBODIES,AT ANGLES OF ATTACK UP TO 180 DEGREE WITH VARIOUS DEGREES OF NOSE BLUNTING.	NASA TN D-1608 AN ANALYTICAL STUDY OF A SIMPLE ATTITUDE CONTROL SYSTEM FOR A FINNED VEHICLE.	NASA TN D-1610 SELF-ERECTING FLEXIBLE FOAM STRUCTURES FOR SPACE ANTENNAS.	NASA TN D-1611 PERFORMANCE AND SOME DESIGN ASPECTS OF THE FOUR-STAGE SOLID-PROPELLANT ROCKET VEHICLE USED IN THE RAM A1 FLIGHT TEST	NASA TN D-1612 PRESSURE DISTRIBUTIONS OVER THE FORWARD PORTION OF THE PROJECT FIRE SPACE-VEHICLE CONFIGURATION AT MACH NUMBER FROM 0.25 TO 0.60	NASA TN D-1613 POLOT-CONTROLLED SIMULATION OF RENDEZVOUS BETWEEN A SPACE CRAFT AND A COMMANDED MODULE HAVING LOW THRUST	NASA TN D-1614 EXPERIMENTAL INVESTIGATION OF THE DYNAMIC STABILITY STABILITY OF A TOWED PARAWING GLIDER MODEL	Next

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