Influence of AP/HTPB flame structure on aluminum behavior in laminate propellents

J. C. Mullen, M. Q. Brewster

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

High speed video imaging of aluminum and surface flame structure in ammonium perchlorate/hydroxyl-terminated poiybutadlene (AP/HTPB) laminate propellants was used to characterize the influence of AP/HTPB flame structure on aluminum behavior in these oxtdizer/hydrocarbon laminates. Spherical aluminum powder, nominally 15 μm, intermixed with 76/24 (mass ratio) 2 μm AP/HTPB was used as the fuel layer between two AP slabs. Fuel layer thicknesses ranging from 0.25 mm to 1.25 mm and pressures of 3 atm to 30 atm were investigated. Video images indicated a non-protruded surface layer for all conditions tested including thick fuel layers for which non-aluminized laminates showed a protruding fuel layer. Similar to non-aluminized laminates, Increased pressure and fuel layer thickness resulted in a transition in flame structure from merged (premixed) to split (diffusion). Ignition of aluminum occurred in the stoichiometric AP/HTPB diffusion flame where adiabatic flame temperatures were suitable for oxide layer cracking or melting. Due to lack of surface protrusion (which was used for non-aluminized laminates), the criterion for merged vs. split flame AP/HTPB flame structure was based on traces of alumina smoke produced by aluminum ignition and combustion. Laminate burning rate increased with increasing pressure but remained relatively constant with fuel layer thickness. This was in contrast to non-aluminized laminates that showed a clear optimum burning rate at conditions where the diffusion flames merge. Aluminum agglomerate size typically ranged between 25-40 μm.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
Pages5717-5726
Number of pages10
StatePublished - Dec 1 2006
EventAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference - Sacramento, CA, United States
Duration: Jul 9 2006Jul 12 2006

Publication series

NameCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
Volume7

Other

OtherAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
CountryUnited States
CitySacramento, CA
Period7/9/067/12/06

Fingerprint

ammonium perchlorates
perchlorate
laminates
Laminates
flames
ammonium
aluminum
Aluminum
burning rate
diffusion flames
ignition
Ignition
Adiabatic flame temperature
flame temperature
smoke
propellants
Propellants
Smoke
mass ratios
aluminum oxide

ASJC Scopus subject areas

  • Space and Planetary Science
  • Energy(all)
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

Cite this

Mullen, J. C., & Brewster, M. Q. (2006). Influence of AP/HTPB flame structure on aluminum behavior in laminate propellents. In Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference (pp. 5717-5726). (Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference; Vol. 7).

Influence of AP/HTPB flame structure on aluminum behavior in laminate propellents. / Mullen, J. C.; Brewster, M. Q.

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference. 2006. p. 5717-5726 (Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference; Vol. 7).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Mullen, JC & Brewster, MQ 2006, Influence of AP/HTPB flame structure on aluminum behavior in laminate propellents. in Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference. Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference, vol. 7, pp. 5717-5726, AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference, Sacramento, CA, United States, 7/9/06.
Mullen JC, Brewster MQ. Influence of AP/HTPB flame structure on aluminum behavior in laminate propellents. In Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference. 2006. p. 5717-5726. (Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference).
Mullen, J. C. ; Brewster, M. Q. / Influence of AP/HTPB flame structure on aluminum behavior in laminate propellents. Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference. 2006. pp. 5717-5726 (Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference).
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