NASA SBIR 2014 Solicitation

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Creare, Inc.
P.O. Box 71
Hanover, NH 03755 - 3116
(603) 643-3800

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Michael Izenson
mgi@creare.com
P.O. Box 71
Hanover, NH 03755 - 3116
(603) 643-3800 Extension :2405

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Robert Kline-Schoder
contractsmgr@creare.com
P.O. Box 71
Hanover, NH 03755 - 3116
(603) 643-3800 Extension :2487

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 4

Technology Available (TAV) Subtopics
Space Suit Pressure Garment and Airlock Technologies is a Technology Available (TAV) subtopic that includes NASA Intellectual Property (IP). Do you plan to use the NASA IP under the award?
No

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
Future manned space exploration missions will require space suits with capabilities beyond the current state of the art. Portable Life Support Systems for these future space suits face daunting challenges, since they must maintain healthy and comfortable conditions inside the suit for long-duration missions while minimizing weight and water venting. We propose to develop an innovative, multipurpose garment for thermal and humidity control inside a space suit pressure garment that is simple, rugged, compact, and lightweight. Our approach is to make simple modifications to a conventional liquid cooling and ventilation garment (LCVG) so that it can directly absorb latent heat as well as sensible heat. This hybrid garment will prevent buildup of condensation inside the pressure garment, prevent loss of water by absorption in regenerable CO2 removal beds, and conserve water through use of Creare's lithium chloride absorber/radiator (LCAR) technology for nonventing heat rejection. In Phase I we will prove the feasibility of our approach by sizing the critical components for the hybrid garment, developing fabrication methods, building and testing a proof-of-concept system, and demonstrating by test that its performance is suitable for use in space suit life support systems. In Phase II we will optimize the overall design for integration with space suit systems, produce a full-size prototype garment, and demonstrate operation in a prototypical environment.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed system can be used in any future space suit, with applications that include near-Earth asteroids and Mars moons as well as lunar and Martian surface missions. The basic technology can also be used to provide rugged, nonventing thermal and humidity control for spacecraft, manned rovers, and habitats.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
There are numerous commercial and military applications for the proposed technology. Commercial applications include untethered personal cooling systems for law enforcement, nuclear/chemical plant workers, and heat-sensitive multiple sclerosis patients. Military applications include personal cooling systems for soldiers or marines wearing chem/bio protective gear, body armor, EOD suits, or level-A HAZMAT suits.