NASA SBIR 2014 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 14-1 S3.02-9912
SUBTOPIC TITLE: Propulsion Systems for Robotic Science Missions
PROPOSAL TITLE: Low-Cost and High-Performance Propulsion for Small Satellite Applications

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
Ventions, LLC
1142 Howard Street
San Francisco, CA 94103 - 3914
(415) 543-2800

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Adam London
adam.london@ventions.com
1142 Howard Street
San Francisco, CA 94103 - 3914
(415) 543-2800

CORPORATE/BUSINESS OFFICIAL (Name, E-mail, Mail Address, City/State/Zip, Phone)
Amit Mehra
amit.mehra@ventions.com
1142 Howard Street
San Francisco, CA 94103 - 3914
(202) 213-2846

Estimated Technology Readiness Level (TRL) at beginning and end of contract:
Begin: 2
End: 4

Technology Available (TAV) Subtopics
Propulsion Systems for Robotic Science Missions 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)
While small satellites continue to show immense promise for high-capability and low-cost missions, they remain limited by post-deployment propulsion for a variety of activities like precision maneuvering, orbit change and controlled re-entry / recovery. Furthermore, any on-board propulsion system capable of providing sufficiently high delta-V is likely to impose constraints on handling, storage, operations and safety that may limit consideration as a secondary payload. Ventions proposes to overcome these limitations by developing a compact, light-weight and low-cost 3U cubesat propulsion system that uses non-toxic propellants to provide approximately 125m/sec of delta-V within a 1kg and 100mm x 100mm x 100mm mass and size budget.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Currently, since all NASA cubesats are manifested as secondary payloads on launch vehicles carrying a large satellite, their deployment location is limited by the orbit characteristics of the primary payload. This greatly constrains the ability to deploy a highly-functional cubesat in a desired location to obtain "high-value science" from low-cost small spacecraft. Availability of the proposed on-board propulsion system is expected to enable significant post-deployment maneuverability, thereby allowing for much-needed orbit phasing and drag makeup capability to achieve several application-specific goals (e.g. science return).

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The proposed on-board propulsion capability is also expected to allow for controlled re-entry and recovery for cubesats from orbits as high as 450km, and to enable orbit changing maneuvers in very small NRO-class missions (e.g., rapidly distributing a constellation around an orbital plane, changing overpass time of a given location in a sun-synchronous orbit, or lowering the perigee of an orbit over a particular latitude "on-demand" to enable improved resolution for reconnaissance missions).

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.)
Maneuvering/Stationkeeping/Attitude Control Devices

Form Generated on 04-23-14 17:37