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HELICOPTER-ENGINE ACCELERATION-TIME REQUIREMENTS BASED ON PILOT DEMAND DURING RECOVERY FROM LANDING FLAREOUTS

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BookPublisher: Nasa, Washington, D.C. 1960Description: 11.DDC classification: NASA | TN D-370

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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-370 (Browse shelf)	Not for loan		TR16264

Total holds: 0

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Previous	NASA TN D-3697 - SUMMARY OF LIGHT-INTENSITY DATA OF EIGHT TRAILBLAZER I REENTRY BODIES	NASA TN D-3698 - SOME EFFECTS OF JET PLUMING ON THE STATIC STABILITY OF BALLISTIC BODIES AT A MACH NUMBER OF 6.00	NASA TN D-3699 - ANALYSIS OF USE JUPITER GRAVITY TURNS FOR TAILORING TRAJECTORIES TO SATURN WITH CONSIDERATION OF LAUNCH OPPORTUNITIES	NASA TN D-370 HELICOPTER-ENGINE ACCELERATION-TIME REQUIREMENTS BASED ON PILOT DEMAND DURING RECOVERY FROM LANDING FLAREOUTS	NASA TN D-3700 - TRANSONIC AERODYNAMIC INVESTIGATION OF TENSION SHELL AND BLUNTED 100(DEGREE) CONICAL SHAPES FOR UNMANNED ENTRY VEHICLES	NASA TN D-3702 BENDING TESTS OF TWO LARGE-DIAMETER CORRUGATED CYLINDERSM WITH ECCENTRIC RING STIFFENERS.	NASA TN D-3703 NAVIGATION ACCURACY FOR INFRARED ESQUIPPED APOLLO AIRCRAFT FOR REENTRY TRACKING.	Next

Bound With Nasa Tn D-361-369

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