SBIR-STTR Award

Hardware Component Prototyping for Operationally Responsive Space Access
Award last edited on: 7/12/2007

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$849,539
Award Phase
2
Solicitation Topic Code
AF071-260
Principal Investigator
Dan DeLong

Company Information

XCOR Aerospace Inc

325 Sabovich Street
Mojave, CA 93501
   (661) 824-4714
   info@xcor.com
   www.xcor.com
Location: Single
Congr. District: 23
County: Kern

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
2007
Phase I Amount
$99,935
XCOR's proposal is to build and fly a rocket powered vehicle that will fly near space, and measure its operational responsiveness. We are proposing to build the simplest possible all-rocket powered vehicle that will get to 200,000 ft altitude and supersonic speeds. We plan to complete vehicle fabrication during Phases I and II with matching private investment money. This vehicle will build on a legacy of XCOR's previous private and government technology investments, including reusable liquid rocket engines that are capable of hundreds of restarts, piston propellant pumps, low cost highly reliable valves, rapid propellant filling techniques, and proven reliable ignition systems.

Keywords:
Ors, Operationally Responsive, Reuseable, Rocket-Powered, Supersonic, Testbed

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
2008
Phase II Amount
$749,604
XCORÂ’s Air Force-funded work under the Phase II contract will focus on augmenting existing commercial vehicle development program to implement AFRL/VA Operationally Responsive Space (ORS) technologies including ground demonstrations and other activities. This will include the insertion of specific AFRL ORS technologies and vehicle design features into XCOR's Minimal Supersonic Vehicle (MSV). XCOR Aerospace proposes a partnership to enable reliable, rapid access, low cost demonstrations of ORS technologies. XCOR is developing, using already-secured private funds, a suborbital RLV for commercial applications. This gives AFRL huge potential leverage for ORS technology development and demonstration in several distinct ways. First, some of the final development work planned for the vehicle is directly relevant to Air Force ORS goals and systems. Second, additional work that could be carried out during development will augment the baseline development effort and further support these goals. Third, once the vehicle is flying, it will be able to collect real-world systems operability and flight test data for AFRL. Fourth, the vehicle will be able to conduct spacecraft testing and checkout for a variety of potential intelligence, surveillance, reconnaissance, and communications related R&D projects.

Keywords:
Ors, Operationally Responsive, Reuseable, Rocket-Powered, Spacelift, Supersonic, Testbed