Accession Number:

AD0353781

Title:

PULSED ROCKET VELOCITY CONTROL FINAL PROGRAM REPORT

Descriptive Note:

Rept. for 1 Mar 62-31 Jul 63,

Corporate Author:

CHRYSLER CORP DETROIT MI MISSILE DIV

Report Date:

1964-08-10

Pagination or Media Count:

66.0

Abstract:

The concept of pulsed rocket velocity control is defined as well as its integration with a total missile system. The research, development and testing are summarized. Test results, conclusions and recommendations are included. A Pulsed Rocket Velocity Control System was breadboarded and tested. Twenty-three static tests were made to evaluate the pulsed mode of operation. Computer flight simulations were made to determine operational characteristics and the effects of experimentally determined time delays. Author

Subject Categories:

  • Reciprocating and Rotating Engines
  • Liquid Propellant Rocket Engines

Distribution Statement:

APPROVED FOR PUBLIC RELEASE