Method for generating rocket motor data profiles for firings...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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C102S202000, C102S501000, C434S012000, C434S014000

Reexamination Certificate

active

07024288

ABSTRACT:
A method for generating predictions of rocket motor ballistic performance at specific firing temperatures and for generating data profiles for analysis. The method requires generally available specifications for the rocket motor to be tested and test data from one or more test firings at a known temperature. The method is implemented in software form and generates pressure and thrust versus time data at a selected temperature. The method generates a burnback profile with a correct final web that integrates to the correct final propellant weight as well as a throat area profile and thrust coefficient profile, for the test firing temperature and for the temperature to be predicted.

REFERENCES:
patent: 6290505 (2001-09-01), Garcia
patent: 6317658 (2001-11-01), Vian
NACA Research Memorandum:By Sanford Gordon and Vearl N. Huff. Theoretical Performance of Lithium and Fluorine as a Rocket Propellant, May 10, 1951—AeroPocket.com Technology; Rocket Motor Test Stand(RMTS).

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