Dual Use Catalytically Initiated Combustor (CIC) for Rocket Engine Ignition and Thruster Applications

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$99,257.00
Award Year:
2011
Program:
SBIR
Phase:
Phase I
Contract:
NNX11CE05P
Agency Tracking Number:
105966
Solicitation Year:
2010
Solicitation Topic Code:
O2.02
Solicitation Number:
n/a
Small Business Information
K T Engineering Corporation
238 Business Park Boulevard, Building 23B Suite J, Madison, AL, 35758-7552
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
127963515
Principal Investigator:
Greg Saks
Principal Investigator
(256) 461-8522
greg.saks@kte-aerospace.com
Business Contact:
David Sisk
Business Official
(256) 461-8522
dave.sisk@kte-aerospace.com
Research Institution:
Stub




Abstract
This proposal responds to subtopic O2.02 "Propulsion Technologies" and the stated need to develop component technologies that will lead to future propulsion systems that are reliable and have adequate performance without requiring excessive specialized handling equipment and procedures or needing to push materials and designs to the limits of their capabilities. We propose the development of a low part count and low energy Catalytically Initiated Combustor (CIC) that can serve as a rocket engine igniter as well as the basis for a family of low cost and highly reliable launch vehicle and satellite thrusters. We propose a 6-month Phase I program to 1) demonstrate reliable ignition and operation of our baseline CIC with hydrogen, methane, and propane fuels, 2) demonstrate reliable ignition and operation of our baseline CIC under cold gas inlet conditions, 3) demonstrate extended duration hot fire testing and durability of our CIC design over multiple ignition cycles, and 4) demonstrate rapid pulsed operation necessary for a launch vehicle or space craft thruster application. Under our proposed Phase I effort, we will also conduct a market survey of potential customers and define a flight weight CIC with maximum commercial utility as either an igniter or small thruster.

* information listed above is at the time of submission.

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