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Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics [NASA CR-1901]

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BookSeries: National Aeronautics and Space Administration(NASA ). Publisher: Waahington, D.C. NASA 1971Description: xvi, 167p.Subject(s): V/STOL aircraft | V/STOL descent angle limiations | V/STOL Flight dynamicsDDC classification: NASA | CR-1901

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	Reference	NASA CR-1901 (Browse shelf)	Not for loan		101558

Total holds: 0

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Previous	NASA CR-1638 - EXPERIMENTAL AND ANALYTICAL INVESTIGATIONS ON MULTIPLE LIQUID IMPACT EROSION [NASA CR- 1638]	NASA CR-1639 INELUENCE OF SUCTION ON SHOCK WAVE-TURBULENT BOUNDARY LAYER INTRACTION FOR TWO-DIMENSIONAL AND AXIALLY SYMMETRIC FLOWS [NASA CR-1639]	NASA CR-1640 A FURTHER STUDY OF JIMSPHERE WIND PROFILES AS RELATED TO SPACE VEHICLE DESIGN AND OPERATIONS[NASA CR-1640]	NASA CR-1901 Fundamental limitations on V/STOL terminal guidance due to aircraft characteristics [NASA CR-1901]	NASA CR-1902 ATTITUDE-REFERENCED RADIOMETER STUDY- Part II- primary calibration System [NASA CR-1902]	`NASA CR-1905 IMPROVED NEUTRON ACTIVATION PREDICTION CODE SYSTEM DEVELOPMENT [NASA CR-1905]	NASA CR-1907 SNAP-8 ELECTRICAL GENERATING SYSTEM DEVELOPMENT PROGRAM [NASA CR-1907]	Next

Bound with NASA CR- 1901-08( Bound Acc. No.101558)

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