Reduction of Flash X-Ray Data of Rocket Motors to Obtain Propellant Burning Rate Profiles

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Authors
  1. Gottlieb,J.J.
  2. Greatrix D.R.
Corporate Authors
Defence R&D Canada - Valcartier, Valcartier QUE (CAN);Toronto Univ, Toronto ONT (CAN) Inst for Aerospace Studies
Abstract
The reduction of flash X-ray data of burning rocket motors to obtain the regression rate of the burning propellant surface at various times during a rocket motor firing is presented herein. All data reduction techniques, final data, and their analyses are reported, followed by a discussion of the results and an assessment of the techniques and data.
Keywords
Flash X-Rays
Report Number
DRDC-VALCARTIER-CR-2003-352 — Contractor Report
Date of publication
01 Nov 1986
Number of Pages
271
DSTKIM No
CA023260
CANDIS No
520521
Format(s):
Hardcopy;Document Image stored on Optical Disk

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