Normal view MARC view ISBD view

EXPERIMENTAL PERFORMANCE OF AN ION ROCKET ENGINE USING A RECTANGULAR-SLAB POROUS-TUNGSTEN EMITTER

Material type: materialTypeLabel

BookPublisher: Nasa, Washington, D.C. 1962Description: 26.DDC classification: NASA | TN D-1321

average rating: 0.0 (0 votes)

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-1321 (Browse shelf)	Not for loan		65531

Total holds: 0

Previous								Next
Previous	NASA TN D-1318 PERFORMANCE OF SEVERAL CAST NICKLE-BASE ALLOYS AS TURBOJET-ENGINE BUCKET MATERIALS AT 1650 DEGREE F.	NASA TN D-1319 THREE-DIMENSIONAL TRAJECTORY ANALYSIS FOR ROUND-TRIP MISSION TO VENUS.	NASA TN D-1320 A CENTRAL FACILITY FOR RECORDING AND PROCESSING TRANSIENT-TYPE DATA .	NASA TN D-1321 EXPERIMENTAL PERFORMANCE OF AN ION ROCKET ENGINE USING A RECTANGULAR-SLAB POROUS-TUNGSTEN EMITTER	NASA TN D-1322 CRITICALITY EFFECTS OF CENTRALLY LOCATED TUBES AND RODS OF ALUMINUM,IRON,AND TUNGSTEN IN A HOMOGENEOUS REACTOR	NASA TN D-1323 NUMERICAL SOLUTION OF TWO -DIMENSIONAL POISSON EQUATION	NASA TN D-1324 ELECTRON DIFFUSION IN A TURBULENT PLASMA	Next

Bound With Nasa Tn D-1322-1330

There are no comments for this item.

PKK Library