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A STUDY OF THE EFFECTS OF MEASUREMENT ERRORS UPON A RANGE CONTROLLER FOR AN ENTRY VEHICLE.

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BookPublisher: National Aeronautics And Space Administration, Washington, D.C. Description: 32.DDC classification: NASA | TN D-4317

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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-4317 (Browse shelf)	Not for loan Untraceable		TR11336

Total holds: 0

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Previous	NASA TN D-4314 PRESSURE DISTRIBUTIONS AND AERODYNAMIC CHARACTERISTICS OF 9 DEGREE AND 15 DEGREE BLUNTED CONES IN NITROGEN AND HELIUM AT MACH 20.	NASA TN D-4315 PRELIMINARY CONSIDERATIONS FOR FAST-SPECTRUM, LIQUID-METAL COOLED NUCLEAR REACTOR PROGRAM FOR SPACE-POWER APPLICATIONS.	NASA TN D-4316 SUBSONIC AND TRANSONIC FLUTTER AND FLOW INVESTIGATIONS OF THE T-TAIL OF A LARGE MULTIJET CARGO AIRPLANE.	NASA TN D-4317 A STUDY OF THE EFFECTS OF MEASUREMENT ERRORS UPON A RANGE CONTROLLER FOR AN ENTRY VEHICLE.	NASA TN D-4318 EFFECTS OF LONGTIME ENVIRONMENTAL EXPOSURE ON MECHANICAL PROPERTIES OF SHEET MATERIALS FOR A SUPERSONIC TRANSPORT.	NASA TN D-4319 COATINGS AND SURFACE TREATMENTS FOR LONGTIME PROTECTION OF TI-8A1-1M0-IV ALLOY SHEET FROM HOT-SALT STRESS CORROSION.	NASA TN D-432 A SUMMARY OF OPERATING CONDITIONS EXPERIENCED BY THREE MILITARY HELICOPTERS AND A MOUNTAIN-BASED COMMERCIAL HELICOPTER	Next

Bound With Nasa Tn D-4311-16, 4318-20

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