Azimuth (AZ) Motor/Brake Assembly XB Radar System
| Location: |
Federal |
| Posted: |
Apr 9, 2026 |
| Agency: |
DEPT OF DEFENSE |
| Type of Contract: |
Awards |
| Type of Government: |
Federal |
| Category: |
- 58 - Communications, Detection and Coherent Radiation Equipment
|
| Solicitation No: |
FA850726PB001 |
| Publication URL: |
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Azimuth (AZ) Motor/Brake Assembly XB Radar System
Active
Contract Opportunity
Related Notice
FA8507-26-Q-B002
Contract Line Item Number
Department/Ind. Agency
DEPT OF DEFENSE
Sub-tier
DEPT OF THE AIR FORCE
Major Command
AIR FORCE MATERIEL COMMAND
Sub Command
AIR FORCE LIFE CYCLE MANAGEMENT CENTER
Sub Command 2
ELECTRONIC SYSTEMS
Office
FA8507 ALCMC ESKC
Award Details
General Information
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Contract Opportunity Type: Award Notice (Original)
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Original Published Date: Apr 09, 2026 01:17 pm EDT
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Inactive Policy: 15 days after contract award date
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Original Inactive Date:
Apr 24, 2026
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Initiative:
Classification
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Original Set Aside: No Set aside used
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Product Service Code: 5840 - RADAR EQUIPMENT, EXCEPT AIRBORNE
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NAICS Code:
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335312 - Motor and Generator Manufacturing
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Place of Performance:
Description
GLOBUS is a classified Joint Program. Maintenance and operation is performed at the OCON US site by personnel employed by the Joint partner. The missions are of a highly specialized nature, utilizing specialty type equipment and requiring highly trained personnel.
This effort is for the procurement of custom motor/brake (P/N 53983-12-3500-01) assemblies for the GLOBUS X-Band Radar system. The Pedestal Control System (PCS) supports the rotational movement of the radar system. The PCS is composed of the servo controls and drive motor/brake assemblies. The AZ Motor/Brake Assembly consists of (brake pre-wiring, clamp collar and motor installation) which must be fully tested after assembly to guarantee it meets specification requirements.
The motor/brake assembly consists of a motor (HP: 55, RPM 3600 with tach, high inertia) and a brake (125 ft-lb, 120 VAC, 50Hz, 256TC, VERT Above). The Brake Assembly Modification (P/N 53983-12-4600-01) is required prior to field installation for the GLOBUS X-Band Subsystem and is proprietary. The brake must be prepared electrically and mechanically to the specs in the Brake Assembly Modification to avoid catastrophic failure and damage. Quality testing and documentation is provided as part of the process.
Attachments/Links
Contact Information
Contracting Office Address
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236 MILLEDGEVILLE ST STE F30
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ROBINS AFB , GA 31098-1670
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USA
Secondary Point of Contact
History
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