SBIR/STTR Research Award

Low Cost, High Efficiency, Pressurization System for Responsive Launch Operations

Award identifier 7786e73e448e9c60cbcebef9dd85800e86035fa9cf2819e657efacfd1438440dAwarding agency National Aeronautics and Space Administration

Award amount

$124,351

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
K T Engineering Corporation
Proposal award date
2012-02-13
Contract end date
2012-08-13
UEI
D48LRKKN8NQ9
Solicitation number
Not reported
Topic code
O2.03

Research abstract

KT Engineering (KTE) is pleased to submit this proposal to address the stated need for "innovative solutions that will allow spaceport launch service providers to operate in an efficient, low cost manner and increases capabilities associated with integration, checkout, and preparations required to configure and ready space systems for launch." We propose to conduct research and demonstrate feasibility of a novel launch vehicle pressurization system concept that will increase performance and reliability compared with traditional approaches, reduce dependence upon helium up to 50%, enable the use of low-cost commercial off the shelf technology, and demonstrate the automated ground processing associated with this technology. Our innovation is based on five major technology and operational elements including: 1) Tridyne Pressurant, 2) Distributed Storage and Control, 3) Cold Gas Storage / Warm Gas Delivery, 4) Bang-Bang Pressure Control, and 5) End-of-burn Tank Pressure Decay. Pump-fed launch vehicles will benefit from our innovative concept but the most significant benefits are achieved in cost-optimized pressure-fed systems such as KT Engineering's Radially Segmented Launch Vehicle (RSLV). We propose a six month Phase I program to refine the designs of the critical ground and airborne elements of this distributed pressurization system. We intend to demonstrate feasibility and more accurately quantify the benefits of our approach through analytical modeling, preliminary design, and high-flow, high-pressure testing of a prototype Tridyne catalytic reactor. The product of this effort will be engineering analysis and models, presentation materials from major reviews, a comprehensive final report, and our Phase II proposal. Under Phase II we will proposed to demonstrate design and operation of the ground and airborne elements of our pressurization system through prototype hardware fabrication and testing in the NASA KSC Launch Equipment Test Facility (LETF).

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

7 SBIR/STTR records share this UEI (2003–2017). Reported award amounts total $1,586,980. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense

Agency intelligence

National Aeronautics and Space Administration

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