NASA SBIR 2015 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 15-1 S3.07-9621
SUBTOPIC TITLE: Thermal Control Systems
PROPOSAL TITLE: High heat flux Enhanced Acquisition and Transport system for Small spacecraft

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
LoadPath
933 San Mateo Boulevard Northeast, Suite 500-326
Albuquerque, NM 87108 - 1862
(866) 411-3131

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Derek Hengeveld Ph.D.
dhengeveld@loadpath.com
933 San Mateo Blvd NE, ste 500-326
Albuquerque, NM 87108 - 1862
(605) 690-1612

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Adam Biskner
abiskner@loadpath.com
933 San Mateo Boulevard NE, Ste 500-326
Albuquerque, NM 87108 - 1862
(505) 331-5331

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 3
End: 5

Technology Available (TAV) Subtopics
Thermal Control Systems 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 small-spacecraft thermal engineers and integrators will contend with increasing spacecraft power and temperature variations resulting from challenging new missions in extreme environments. The LoadPath High heat flux Enhanced Acquisition and Transport system for Small spacecraft (HEATS) is an innovative, passive, two-phase thermal transport system that will help realize these missions of tomorrow. Unlike state-of-the-art thermal transport systems (e.g. heat pipes and loop heat pipes), our approach can mitigate higher heat loads and fluxes at a lower cost and mass while adapting to a wider-range of heat source/sink configurations.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The immediate targeted NASA applications are enabling smaller and lower cost spacecraft capable of conducting valuable scientific measurements with reduced mass and costs. Early development will also target exploration missions that are at or near the surface of planets such as Mars, Europa, and Enceladus. HEATS will facilitate these applications because of is high heat load and flux mitigation, ability to maintain components within a specified temperature range, adaptability and reconfigurability to new missions or a wide-range of heat source/sink configurations, low system cost, and low mass.
The proposed technology impacts a broad array of NASA missions because it will benefit most, if not all, unmanned NASA missions requiring TCS design. The National Research Council Aeronautics and Space Engineering Board identified NASA's top technical challenges and highest priority technologies across all 14 NASA space technology roadmaps. Based on their study, thermal control systems are a key, enabling technology that contributes to the advancement of many of the top technical challenges and the highest priority technologies.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Similarly to NASA unmanned missions, HEATS will be of interest to other Government spacecraft procuring agencies such as the Air Force, Navy, National Reconnaissance Office, and Operationally Responsive Space Office; as well as, prime contractor spacecraft developers such as ATK, Lockheed Martin, Boeing, Northrop Grumman, Sierra Nevada Corporation, and Raytheon. In addition to satellite applications, HEATS will be valuable to thermal management applications where performance, size, and weight are important concerns.

TECHNOLOGY TAXONOMY MAPPING (NASA's technology taxonomy has been developed by the SBIR-STTR program to disseminate awareness of proposed and awarded R/R&D in the agency. It is a listing of over 100 technologies, sorted into broad categories, of interest to NASA.)
Active Systems
Avionics (see also Control and Monitoring)
Cryogenic/Fluid Systems
Distribution/Management
Heat Exchange
Isolation/Protection/Shielding (Acoustic, Ballistic, Dust, Radiation, Thermal)
Passive Systems
Spacecraft Design, Construction, Testing, & Performance (see also Engineering; Testing & Evaluation)

Form Generated on 04-23-15 15:37