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Advanced Solid Axial Stage (ASAS) with Fast ResponseSecondary Hot Gas Injection TVC

Award Information
Agency: Department of Defense
Branch: Missile Defense Agency
Contract: HQ0147-18-C-7435
Agency Tracking Number: B181-004-0067
Amount: $99,988.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: MDA18-004
Solicitation Number: 2018.1
Timeline
Solicitation Year: 2018
Award Year: 2018
Award Start Date (Proposal Award Date): 2018-06-25
Award End Date (Contract End Date): 2018-12-24
Small Business Information
160 Blue Ravine Road, Ste A
Folsom, CA 95630
United States
DUNS: 793187670
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Russell Carlson
 (707) 696-5354
 russ.carlson@vts-i.com
Business Contact
 Joe Viola
Phone: (916) 990-8736
Email: joe.viola@vts-i.com
Research Institution
N/A
Abstract

The United States has fielded a layered missile defense system to counter and defeat current hostile missile threats. However, evolving adversarial capabilities requires new propulsion technologies that are highly responsive, agile and compatible to current MDA interceptor platforms. To meet this evolving need, Valley Tech Systems (VTS) is proposing the development of a high performance Affordable Solid Axial Stage (ASAS) for flexible high-G Delta-v impulse control and fast Thrust Vector response times. Our development approach applies the VTS extensive controllable solid propulsion Hot Gas Valve technology to a new high-performance booster hot-gas injection (HGI) Thrust Vector Control (TVC) design minimizing state of the art axial stage propulsion Size, Weight and Power (SWaP).During the phase I program VTS will conduct advanced ASAS concept design activities and conduct a subscale hot gas demonstration of a prototype HGI nozzle assembly. During the Phase II program a full scale ASAS prototype booster assembly will be developed and tested maturing the technology to TRL 4/5.Approved for Public Release | 18-MDA-9710 (6 Jul 18)

* Information listed above is at the time of submission. *

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