Velocities of Reacting Boron Particles within a Solid Fuel Ramjet Combustion Chamber

  • J. Sender DLR, German Aerospace Centre,Germany.
  • H.K. Ciezki DLR, German Aerospace Centre , Germany
Keywords: Velocimeter, Laser doppler

Abstract

A 2D-laser doppler velocimeter was used to measure velocities of reacting boron (B) particles during the combustion of a metallised solid fuel slab inside a 20-combustion chamber. The solid fuel hydroxyl-terminated polybutadiene (HTPB) was enriched with B particles to increase its specific heat. To obtain information on the combustion process and on the movement of B particles, their velocities were measured. The experiments were performed at ambient pressure. The behaviour of the B particles concerning the exit velocities from the fuel slab has been discussed on the basis of the experimental results.

Author Biographies

J. Sender, DLR, German Aerospace Centre,Germany.
Mr J Sender studied Chemical Engineering at the University of Erlangen/N"urnberg, Germany. He has worked on several engineering and scientific projects at the Institute of Fluid Mechanics of the University Erlangen/N"urnberg. Presently, he is Head, Spray Combustion Group at DLR, German Aerospace Centre. His areas of research include cryogenic combustion of hydrogen/oxygen. He is a member of the Optical Diagnostics Group of German Aerospace Centre, in Lampoldshausen.
H.K. Ciezki, DLR, German Aerospace Centre , Germany
DLR, German Aerospace Centre , Germany
Published
2013-01-01
How to Cite
Sender, J., & Ciezki, H. (2013). Velocities of Reacting Boron Particles within a Solid Fuel Ramjet Combustion Chamber. Defence Science Journal, 48(4), 343-349. https://doi.org/10.14429/dsj.48.3958
Section
Aeronautical Systems