Advanced Materials and Cooling Schemes for Rocket Engine Combustion Chambers

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$100,000.00
Award Year:
2001
Program:
SBIR
Phase:
Phase I
Contract:
F04611-00-C-0059
Agency Tracking Number:
001PR3152
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
MATERIALS & ELECTROCHEMICAL RESEARCH
7960 S. Kolb Rd., Tucson, AZ, 85706
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
147518286
Principal Investigator:
Eugene Veksler
Senior Scientist
(520) 574-1980
mercorp@mercorp.com
Business Contact:
R.O. Loutfy
President
(520) 574-1980
rloutfy@mercorp.com
Research Institution:
n/a
Abstract
Proposed enhancement of the thermal control of rocket engine combustion chambers is achieved by implementing advanced high thermal conductivity, light weight polycapillary materials (APM) to provide improved transpiration cooling of the walls and/ordevelop efficient ablative chamber wall material. MER Corporation has developed the method of fabricating metal and/or ceramic APM characterized by: oriented structure of pores/microchannels with sizes varying from tens of microns and up; stability oftheir size along the length at high length-to-diameter ratio (>1000); controlled distribution of pores/microchannels over the various shape cross-section; possibility of using materials of which highly porous products are rarely produced by conventionalmethods. This method involves commonly available equipment and allows to inexpensively produce a variety of APM structures at reasonable cost. During the proposed Phase I effort, MER will team with Aerojet to identify current status of combustion chamber material properties and cooling approaches, and evaluate the feasibility of using APM for transpiration cooling of higher performing hydrogen/oxygen rocket engine combustion chambers as well as using APM for developing high efficiency ablativematerials/liners for chamber walls. Based on evaluation results viable conceptual designs will be formulated.

* information listed above is at the time of submission.

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