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LUNAR ESCAPE SYSTEMS (LESS) FEASIBILITY STUDY

By: Matzenauer,J O.

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BookPublisher: Nasa, Washington, D.C. 1970DDC classification: NASA | CR-1620

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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 CR-1620 (Browse shelf)	Not for loan		TR7797

Total holds: 0

Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: General Stacks Close shelf browser

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Previous	NASA CR-1617 - THERMODYNAMIC PROPERTY MEASUREMENTS IN REFLECTED SHOCK AIR PLASMAS AT 12 - 16,000(DEGREE)K	NASA CR-1618 - ACOUSTIC TESTS OF A FLEXIBLE SPACECRAFT MODEL	NASA CR-1619 LUNAR ESCAPE SYSTEMS (LESS) FEASIBILITY STUDY	NASA CR-1620 LUNAR ESCAPE SYSTEMS (LESS) FEASIBILITY STUDY	NASA CR-1623 - FACTORS AFFECTING THE PERFORMANCE OF POROUS STRUCTURES USED AS OXYGEN FUEL CELL ELECTRODES	NASA CR-1624 - INVESTIGATION OF NOISE CHARACTERISTICS AND AMPLITUDE STABILIZATION OF PLASMA LASERS	NASA CR-1626 - NEW APPROACH TO AERIAL COMBAT GAMES	Next

Bound With Nasa Cr-1616-20

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