An assessment of homogeneous catalysis for the rapid decomposition of hydrogen peroxide
An assessment of homogeneous catalysis for the rapid decomposition of hydrogen peroxide
Liquid catalysts for decomposing hydrogen peroxide in rocket engines have certain advantages over conventional gauzes or pellets. The most potent liquid agents for achieving this decomposition are the permanganates. However, permanganates have a tendency to precipitate at the outlet to the injector and this militates against their use for multiple engine restarts. Against this background, the authors have investigated the feasibility of using different liquid agents to achieve the rapid decomposition needed for use in both monopropellant and bipropellant rocket applications. The results to date suggest that it is unlikely that any of the candidate agents considered will match the performance of the permanganates. However, at least one of the agents (sodium iodide) was found to initiate a very high decomposition rate, albeit with an undesirable initial delay. It was found that ferrous chloride tetrahydrate had no such delay and was capable of producing useful decomposition temperatures.
Musker, A.J.
2458b670-f376-434a-89b3-1202378170a9
Roberts, G.T.
deaf59ac-e4ee-4fc2-accf-df0639d39368
Horabin, R.
ef5b3ae4-7788-49db-bae6-b5b7cb2c9ef0
Kawar, A.
afe987a3-a723-46e8-8a60-c5ecc26d0a40
Payne, M.
fa5f9e34-b209-4ea0-a065-73aa0b9a3d17
Pollard, M.
172acf2b-a2d9-4efb-a3d5-bc3c56b50e89
Ryan, C.
affa16e6-adfb-4339-9d69-9acedbbc140e
July 2006
Musker, A.J.
2458b670-f376-434a-89b3-1202378170a9
Roberts, G.T.
deaf59ac-e4ee-4fc2-accf-df0639d39368
Horabin, R.
ef5b3ae4-7788-49db-bae6-b5b7cb2c9ef0
Kawar, A.
afe987a3-a723-46e8-8a60-c5ecc26d0a40
Payne, M.
fa5f9e34-b209-4ea0-a065-73aa0b9a3d17
Pollard, M.
172acf2b-a2d9-4efb-a3d5-bc3c56b50e89
Ryan, C.
affa16e6-adfb-4339-9d69-9acedbbc140e
Musker, A.J., Roberts, G.T., Horabin, R., Kawar, A., Payne, M., Pollard, M. and Ryan, C.
(2006)
An assessment of homogeneous catalysis for the rapid decomposition of hydrogen peroxide.
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, CA, USA.
08 - 11 Jul 2006.
Record type:
Conference or Workshop Item
(Paper)
Abstract
Liquid catalysts for decomposing hydrogen peroxide in rocket engines have certain advantages over conventional gauzes or pellets. The most potent liquid agents for achieving this decomposition are the permanganates. However, permanganates have a tendency to precipitate at the outlet to the injector and this militates against their use for multiple engine restarts. Against this background, the authors have investigated the feasibility of using different liquid agents to achieve the rapid decomposition needed for use in both monopropellant and bipropellant rocket applications. The results to date suggest that it is unlikely that any of the candidate agents considered will match the performance of the permanganates. However, at least one of the agents (sodium iodide) was found to initiate a very high decomposition rate, albeit with an undesirable initial delay. It was found that ferrous chloride tetrahydrate had no such delay and was capable of producing useful decomposition temperatures.
This record has no associated files available for download.
More information
Published date: July 2006
Additional Information:
AIAA paper 2006-4545
Venue - Dates:
42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, CA, USA, 2006-07-08 - 2006-07-11
Organisations:
Aerodynamics & Flight Mechanics
Identifiers
Local EPrints ID: 49002
URI: http://eprints.soton.ac.uk/id/eprint/49002
PURE UUID: 5fecfece-cac3-40d4-8dcf-020468d3df2e
Catalogue record
Date deposited: 19 Oct 2007
Last modified: 11 Dec 2021 16:52
Export record
Contributors
Author:
A.J. Musker
Author:
R. Horabin
Author:
A. Kawar
Author:
M. Payne
Author:
M. Pollard
Author:
C. Ryan
Download statistics
Downloads from ePrints over the past year. Other digital versions may also be available to download e.g. from the publisher's website.
View more statistics