Accession Number:

AD0374687

Title:

ENGINEERING PROPERTY DATA ON ROCKET PROPELLANTS.

Descriptive Note:

Quarterly rept. no. 1, 1 Apr-30 Jun 66,

Corporate Author:

ROCKETDYNE CANOGA PARK CALIF

Report Date:

1966-07-01

Pagination or Media Count:

46.0

Abstract:

The first quarter-years effort of a 24-month analytical and experimental extension of a previous program, designed to characterize essential propellant properties, is presented in three phases. In Phase 1, the continuous documentation of current propellant properties data is being maintained through a literature survey. Experimental efforts under Phase 2 have resulted in measurements of CH32N2H2 thermal conductivity, ClF5 sonic velocity, CH32N2H2 specific heat, ClF3 phase properties in the critical region and N2 g solubility in ClF5. In addition, assembly of an apparatus to be used in ClF5 viscosity measurements has been completed. Phase 3 efforts resulted in preparation of a bibliography of B2H6 physico-chemical properties. Author

Subject Categories:

  • Rocket Propellants
  • Liquid Rocket Propellants

Distribution Statement:

APPROVED FOR PUBLIC RELEASE