SBIR-STTR Award

Long Life, Fault Tolerant, Spacecraft Sensor Gimbal/Bearing System
Award last edited on: 4/5/02

Sponsored Program
SBIR
Awarding Agency
DOD : AF
Total Award Amount
$99,639
Award Phase
1
Solicitation Topic Code
AF98-089
Principal Investigator
David J Carroll

Company Information

Airex Corporation

15 Lilac Lane
Somersworth, NH 03878
   (603) 841-2040
   connect@airex.comwithapresencein
   www.airex.com
Location: Multiple
Congr. District: 01
County: Strafford

Phase I

Contract Number: F29601-98-C-0118
Start Date: 4/30/98    Completed: 4/9/99
Phase I year
1998
Phase I Amount
$99,639
Current DoD sensor systems employ mechanical bearings in their gimbals to provide slow scan functionality. Mechanical bearings inherently possess a finite life and commonly suffer decreased reliability due to mechanical wear, excessive vibration and inadequate lubrication. The vacuum and temperature extremes of space provide significant technical challenges to these devices in life and pointing accuracy requirements due to stiction and non-repeatable runouts. Furthermore, they are completely unable to provide any vibration isolation to sensitive payloads.Recent advances in electromagnetic suspension and drive technology clearly lend themselves to application for significant improvement in gimbal mounting, promising greater gimbal life, lower weight and power, fault tolerance and vibration isolation. In particular, Airex Corporation, in a previous Phase I effort, has recently demonstrated the viability of two axis pointing using an electromagnetic suspension and integral motor bearing technology. Further, Airex has shown that integral motor-bearings, which use a single electromagnetic actuator to perform both the bearing and rotary pointing (motoring) functions, point the way to new gimbals that are highly reliable, low power, lubricant free, and long life. Such functional sophistication from a novel technology can expand performance in space-borne platforms from commercial or military spacecraft in communications, pointing or optical links.

Phase II

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Start Date: 00/00/00    Completed: 00/00/00
Phase II year
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