Design Factors for Liquid Hydrogen Rocket Engine Test Facilities AETRON, Div. of Aerojet-General Corporation

Format:

Conference/Event

Author/Creator:

Folkerts, K. D., author.

Conference Name:

National Aeronautic and Space Engineering and Manufacturing Meeting (Los Angeles, Calif.)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1963

Summary:

Thermodynamic properties of liquid hydrogen and their relationship to the design of rocket engine test facilities are presented. Major points covered are the need to completely define the thermodynamic state of the liquid, and a method of determining the heat gain during flow from the environment and from fluid friction. Charts useful for estimating these effects are included

Notes:

Vendor supplied data

Publisher Number:

630373

Access Restriction:

Restricted for use by site license