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A HIGH-PERFORMANCE 250-POUND-THRUST ROCKET ENGINE UTILIZING GOAXIAL-FLOW INJECTION OF JP-4 FUEL AND LIQUID OXYGEN

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BookPublisher: Nasa, Washington, D.C. 1959Description: 14.DDC classification: NASA | TN D-126

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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-126 (Browse shelf)	Not for loan		TR15634

Total holds: 0

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Previous	NASA TN D-1249 STATISTICAL WIND DISTRIBUTION DATA FOR USE AT NASA WALLOPS STATION	NASA TN D-125 THERMAL-STRESS FATIGUE GRACKING OF TURBINE BUCKETS OPERATED AT 1700(DEGRE) F IN A TURBOJET ENGINE WITH FREQUENT STARTS AND STOPS	NASA TN D-1250 SUBSONIC WIND-TUNNEL INVESTIGATION OF ERRORS INDICATED BY TOTAL-PRESSURE TUBES IN THE FLOW FIELD OF A BODY SIMULATING THE NOSE OF THE X-15 RESEARCH AIRPLANE	NASA TN D-126 A HIGH-PERFORMANCE 250-POUND-THRUST ROCKET ENGINE UTILIZING GOAXIAL-FLOW INJECTION OF JP-4 FUEL AND LIQUID OXYGEN	NASA TN D-1262 STATISTICAL STUDY OF EFFECTS OF INSERTION ERRORS ON ASCENT TRAJECTORIES FOR LUNAR MISSIONS	NASA TN D-1263 EFFECTS OF FOREBODY LENGTH ON THE STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A CANARD AIRPLANE CONFIGURATION WITH A TRAPEZOIDAL ASPECT-RATIO-3 WING	NASA TN D-1264 PRESSURE DISTRIBUTIONS AT MACH NUMBER 2.05 ON A SERIES OF HIGHLY SWEPT ARROW WINGS EMPLOYING VARIOUS DEGREES OF TWIST AND CAMBER	Next

Bound With Nasa Tn D-121-125,127-130

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