Flow system startup of a full-scale simulated nuclear rocket engine

Performance of liquid hydrogen flow system during startup transient of nuclear rocket in full scale simulated engine system

Document ID

19650025799

Document Type

Technical Memorandum (TM)

Authors

Colmery, B. H. (NASA Lewis Research Center Cleveland, OH, United States)

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

Date Acquired

September 2, 2013

Publication Date

January 1, 1965

Subject Category

Report/Patent Number

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

NTRS