SBIR-STTR Award

Ceramic Matrix Composite Materials for Arc Light Hypersonic Tactical Strike
Award last edited on: 12/29/2014

Sponsored Program
SBIR
Awarding Agency
DOD : DARPA
Total Award Amount
$1,845,379
Award Phase
2
Solicitation Topic Code
NASAX7.04-08
Principal Investigator
Michael Beerman

Company Information

Andrews Space Inc (AKA: Andrews Space & Technology)

3415 South 116th Street Suite 123
Tukwila, WA 98168
   (206) 342-9934
   info@andrews-space.com
   www.andrews-space.com
Location: Multiple
Congr. District: 09
County: King

Phase I

Contract Number: N/A
Start Date: 00/00/00    Completed: 00/00/00
Phase I year
2004
Phase I Amount
$100,000
Andrews Space has shown under a recently completed DARPA study for the Long Range Time Critical Strike initiative that a morphing wing hypersonic vehicle that uses deployable aerosurfaces can very effectively extend the range and decrease the time to target for munitions launched within the constraints of existing launch platforms. The key enabling technology is a composite material that is flexible at room temperature but rigidizes when exposed to high temperatures. The result is a wing structure that is able to withstand both the temperatures and aerodynamic loads encountered during the expected flight profile. This revolutionary wing material is the focus of the proposed effort. Andrews Space proposes to increase the technology readiness level (TRL) of the material by testing in simulated heating environments that are representative of those encountered during hypersonic flight operations. The wing material is a fiber-reinforced ceramic matrix composite (CMC) derived from preceramic polymers that is cured to a stable flexible state for long-term compact storage.

Keywords:
Ceramic Matrix Composite, Hypersonic, Extended Range, Arc Light, Morphing Wing, Deployable Wing, Flexible Composite

Phase II

Contract Number: W31P4Q-09-C-0315
Start Date: 4/8/2009    Completed: 4/9/2010
Phase II year
2009
Phase II Amount
$1,745,379
Andrews Space has shown under a recently completed DARPA study for the Long Range Time Critical Strike initiative that a morphing wing hypersonic vehicle that uses deployable aerosurfaces can very effectively extend the range and decrease the time to target for munitions launched within the constraints of existing launch platforms. The key enabling technology is a composite material that is flexible at room temperature but rigidizes when exposed to high temperatures. The result is a wing structure that is able to withstand both the temperatures and aerodynamic loads encountered during the expected flight profile. This revolutionary wing material is the focus of the proposed effort. Andrews Space proposes to increase the technology readiness level (TRL) of the material by testing in simulated heating environments that are representative of those encountered during hypersonic flight operations. The wing material is a fiber-reinforced ceramic matrix composite (CMC) derived from preceramic polymers that is cured to a stable flexible state for long-term compact storage.

Keywords:
Ceramic Matrix Composite, Hypersonic, Extended Range, Arc Light, Morphing Wing, Deployable Wing, Flexible Composite