NASA SBIR 2011 Solicitation

FORM B - PROPOSAL SUMMARY


PROPOSAL NUMBER: 11-2 S1.10-8477
PHASE 1 CONTRACT NUMBER: NNX12CE32P
SUBTOPIC TITLE: Atomic Interferometry
PROPOSAL TITLE: Accelerometer for Space Applications Based on Light-Pulse Atom Interferometry

SMALL BUSINESS CONCERN (Firm Name, Mail Address, City/State/Zip, Phone)
AOSense, Inc.
767 North Mary Avenue
Sunnyvale, CA 94085 - 2909
(408) 735-9500

PRINCIPAL INVESTIGATOR/PROJECT MANAGER (Name, E-mail, Mail Address, City/State/Zip, Phone)
Adam Black
ablack@aosense.com
767 North Mary Avenue
Sunnyvale, CA 94085 - 2909
(408) 735-9500 Extension :604

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

TECHNICAL ABSTRACT (Limit 2000 characters, approximately 200 words)
We propose to build a compact, high-precision single-axis accelerometer based on atom interferometry that is applicable to operation in space environments. Based on our successful Phase I design, the proposed accelerometer emphasizes reliable operation and exceptional acceleration sensitivity. It incorporates several innovative features that make it appropriate for a variety of space-based and terrestrial applications.

Phase II will result in a completed sensor build, including a sensor head, laser system and electronic control system.

Space-based inertial sensors based on atom interferometry are a compelling technology for both technological and scientific applications because of the exceptionally high performance that can be enabled by long interrogation times with cold atoms in a microgravity environment.

POTENTIAL NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
Inertial measurement units based on the proposed accelerometer technology will be applicable to space-based inertial navigation, including navigation around small bodies such as asteroids. Operating as a gravimeter, the proposed design can be used for Earth geoid measurement and gravity tomography of asteroids. An updated version capable of gravity gradiometry will be capable of gravity-compensation of inertial navigation systems, in addition to improved gravity mapping capabilities. The Phase II prototype will serve as a demonstration of several technologies that are relevant for gravity wave detection. Future iterations of the sensor will ultimately enable gravity wave detection missions.

POTENTIAL NON-NASA COMMERCIAL APPLICATIONS (Limit 1500 characters, approximately 150 words)
The Phase II build will result in an accelerometer capable of acceleration sensitivity that is better than current state-of-the-art conventional absolute gravimeters based on free-fall measurements. Several commercial applications requiring earth-based gravimetry could therefore benefit from the sensor design. Seismic studies and geophysical exploration, including gravity mapping of prospective oil fields and mineral deposits, will benefit from the sensor technology. Trades of sensor bandwidth versus sensitivity will enable the design to apply to inertial navigation on a variety of ground vehicle, sea-based and flight platforms.

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.)
Inertial
Inertial (see also Sensors)
Interferometric (see also Analysis)
Navigation & Guidance


Form Generated on 11-06-12 18:12