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THE EQUIPMENTIAL SPACE-SUIT DESIGN CONCEPT AND ITS APPLICATION TO A SPACE-SUIT ELBOW JOINT.

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BookPublisher: Nasa, Washington, D.C. 1969Description: 42.DDC classification: NASA | TN D-5221

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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-5221 (Browse shelf)	Not for loan		TR15286

Total holds: 0

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Previous	NASA TN D-5218 CONCEPTUAL STUDY OF ROCKET-SCRAMJET HYBRID ENGINES IN A LIFTING REUSABLE SECOND STAGE.	NASA TN D-5219 STATIC LONGITUDINAL AERODYNAMIC CHRACTERISTICS OF SOME SUPERSONIC DECELERATOR MODELS AT MACH NUMBERS OF 2.30 AND 4.63.	NASA TN D-5220 AN ANALYSIS OF TERRAIN BIAS ERROR IN PLANETARY RADAR ALTIMETERS.	NASA TN D-5221 THE EQUIPMENTIAL SPACE-SUIT DESIGN CONCEPT AND ITS APPLICATION TO A SPACE-SUIT ELBOW JOINT.	NASA TN D-5222 ON THE PHENOMENON OF THERMOELASTIC INSTABILITY (THERMAL FLUTTER) OF SECTION WITH OPEN CROSS SECTION.	NASA TN D-5223 THERMODYNAMIC PROPERTIES OF LIQUID H2O AND D2O AND THEIR MIXURES.	NASA TN D-5224 EXPERIMENTS ON POWER LOSS IN HERRINGBONE-GROOVED.GAS-LUBRICATED JOURNAL BEARINGS.	Next

Bound With Nasa Tn D-5211-5220,5222-5230.

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