Thermally Initiated Venting Systems (TIVS)

Award Information
Agency:
Department of Defense
Branch
Missile Defense Agency
Amount:
$100,000.00
Award Year:
2007
Program:
SBIR
Phase:
Phase I
Contract:
W9113M-07-C-0090
Award Id:
81748
Agency Tracking Number:
B063-036-0653
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
200 Boston Avenue Suite 1000, Medford, MA, 02155
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
786127522
Principal Investigator:
Marthinusvan Schoor
CEO/CTO
(781) 306-0609
tienie@mide.com
Business Contact:
PetraBotha
Chief Financial Officer
(781) 306-0609
pbotha@mide.com
Research Institute:
n/a
Abstract
Solid Rocket Motor (SRM) self-detonation is an unacceptable and highly dangerous occurrence. A system that would reduce the likelihood of this occurring would be highly beneficial to the Missile Defense Agency (MDA). Mide proposes to design a Thermally Initiated Venting Systems (TIVS) that will decrease the likelihood of SRM premature detonation in its canister. When the temperature and pressure inside an SRM canister rise too high, it can cause the SRM to detonate, possibly resulting in a loss of life. Mide has previously designed and flight qualified a Positive Pressure Relief Valve (PPRV) that is currently in use on the International Space Station. The valve will work on the same principal as the valve used in the space station. Given a rise in pressure or temperature inside the canister above a pre-determined level, the valve will be automatically be triggered open and quickly reduce the pressure inside the canister, helping to prevent premature detonation.

* information listed above is at the time of submission.

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