Burning rate of solid propellant ingredients, Part 2: Determination of burning rate temperature sensitivity

Authors
Atwood, AI Boggs, TL Curran, PO Parr, TP Hanson-Parr, DM Price, CF Wiknich, J
Citation
Ai. Atwood et al., Burning rate of solid propellant ingredients, Part 2: Determination of burning rate temperature sensitivity, J PROPUL P, 15(6), 1999, pp. 748-752
Citations number
6
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF PROPULSION AND POWER
ISSN journal
07484658 → ACNP
Volume
15
Issue
6
Year of publication
1999
Pages
748 - 752
Database
ISI
SICI code
0748-4658(199911/12)15:6<748:BROSPI>2.0.ZU;2-I
Abstract
Once the burning rate as a function of initial temperature has been measure d for a particular material, it is often desirable to report its burning ra te temperature sensitivity as a single value that can then be used in other applications. A few of the obstacles encountered when making the determina tion of burning rate temperature sensitivity, sigma(p), are examined. Burni ng rate temperature sensitivity was evaluated for the neat ingredients AP, HMX, RDX, ADN, CL-20, and HNF.