SBIR-STTR Award

Robust Optical Edge for a Starshade Petal
Award last edited on: 2/8/2017

Sponsored Program
SBIR
Awarding Agency
NASA : JPL
Total Award Amount
$872,446
Award Phase
2
Solicitation Topic Code
S2.01
Principal Investigator
Gregg Freebury

Company Information

Tendeg LLC

686 South Taylor Avenue Suite 108
Louisville, CO 80027
   (303) 929-4466
   N/A
   www.tendeg.com
Location: Single
Congr. District: 02
County: Boulder

Phase I

Contract Number: ----------
Start Date: ----    Completed: ----
Phase I year
2016
Phase I Amount
$122,466
The proposed Phase I program will design and develop an optical edge that can be integrated to a petal structure and meet the precision, ground handling, packaging, launch and on-orbit environmental requirements. There will be an emphasis on optimizing the integration of a micro-thin metal alloy to a low CTE composite substrate. The Ph1 program will include prototyping and testing the optical edge architecture. In addition, deployable optical close-outs at the root of the petal will also be designed.

Phase II

Contract Number: ----------
Start Date: ----    Completed: ----
Phase II year
2017
Phase II Amount
$749,980
The proposed Phase II program will refine and mature the design of the optical edge, optical shield and snubber assemblies within a Starshade petal. Prototypes of each sub-assembly will be built and tested after a rigorous trade study. The final sub-assembly designs will be built and integrated to a complete petal assembly that utilizes flight-like materials and fabrication processes. The full petal assembly will be tested to demonstrate survival to launch packaging and temperature extremes. A segment of a petal will be delivered to NASA JPL for thermal distortion and stability tests. More specifically, the optical edge assembly efforts will address the integration of a micro-thin metal alloy to a low CTE composite substrate and the alignment and handling procedures required to accurately position each segment to the petal structure. The optical shield effort will address opacity, thermal expansion, micrometeoroid mitigation and venting. The snubber effort will address preload, alignment and support for the petals in the furled and launch configuration.