Nuclear rocket simulator tests, flow initiation with no turbine gas tank pressure, 35 PSIA  Run 1

Nuclear rocket simulator tests, flow initiation with no turbine gas tank pressure, 35 PSIA Run 1

Nuclear reactor simulator test - liquid hydrogen run, instrumentation and data acquisition system operational procedure checkout

Document ID

19660002338

Document Type

Technical Memorandum (TM)

Authors

Biesiadny, T. J. (NASA Lewis Research Center Cleveland, OH, United States)

Coltrin, R. J. (NASA Lewis Research Center Cleveland, OH, United States)

Livingood, J. N. B. (NASA Lewis Research Center Cleveland, OH, United States)

Powers, A. G. (NASA Lewis Research Center Cleveland, OH, United States)

Rudey, R. A. (NASA Lewis Research Center Cleveland, OH, United States)

Straight, D. M. (NASA Lewis Research Center Cleveland, OH, United States)

Date Acquired

September 2, 2013

Publication Date

January 1, 1964

Subject Category

Report/Patent Number

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

NTRS