SOURCES SOUGHT
16 -- Replacement Motor for the M134 Minigun
- Notice Date
- 8/21/2007
- Notice Type
- Sources Sought
- NAICS
- 336413
— Other Aircraft Parts and Auxiliary Equipment Manufacturing
- Contracting Office
- Other Defense Agencies, U.S. Special Operations Command, Technical Applications Contracting Office (TAKO), ATTN: AMSAM-TASO-K Lee Boulevard, Building 401, Fort Eustis, VA, 23604-5577, UNITED STATES
- ZIP Code
- 00000
- Solicitation Number
- Reference-Number-M134minigunmotor
- Response Due
- 8/31/2007
- Archive Date
- 12/31/2007
- Description
- The United States Special Operations Command, Technology Applications Contracting Office, has a requirement for a non-electronically controlled motor to replace the current DC M-134 Minigun motor used in aircraft armament subsystems for intermittent duty per MIL-M-8609 Class B. The Government is attempting to lower the amperage requirements at startup of the M-134 DC powered Minigun. Specific Requirements are as follows: Size: No larger than the current motor with a length of 6.75? Weight: 8.2lbs or less with gear head attached. Firing rate: the gun must fire at a rate of 3000 RMP +/- 100 RPM using gear head PT# DMG0072 (NSN 3020-01-507-3873). Interface: Motor must bolt up to the current 3000RPM Gear head PT# DMG0072 (NSN 3020-01-507-3873) and mount on the M-134D with no modification to the weapon system. Electrical: Input voltage ? 28 VDC per MIL-STD-704, Category B Motor to be in accordance with MIL-M-8609. Maximum starting current of 200 amps when tested on the government test stand at Ft. Campbell Kentucky using an aircraft battery charged to aircraft voltage of 28.25VDC. Run current must be less than 50 amps. Connector PT# MS3450W20-22P (NSN 5935-01-172-6470)or equivalent. It must mate with PT# MS3456W20-22S (harness side). Pin Wiring: Pin 'A' is positive DC drive voltage Pin 'E' is negative DC drive voltage Pin 'D' is mini-gun present (this pin needs to be jumpered to Pin ?E' internally in the motor) The Motor must incorporate a connector protection device to protect the threads of the connector IAW TM 9-1005-343-23&P, dated 28 April 2006, pages 0039-14 thru 0039-16 (currently the government uses the Dillon PN M19025(attachment 1)). This exact device is not required but one which serves the same function is required. The connector must remain inside a straight line from the top edge of the 'doubler' to the aft of the motor housing. Note: Attachment(s) are downloaded to the FedBizOpps website with this notice. Interested vendors should submit their response to this notice by 2:00PMest on 31 August 2007 to Shirley Powell via email, shirley.powell@us.army.mil and to Dan Short at drsfantomworks@verizon.net.
- Place of Performance
- Address: unknown
- Zip Code: 99999
- Country: UNITED STATES
- Zip Code: 99999
- Record
- SN01380259-W 20070823/070822071743 (fbodaily.com)
- Source
-
FedBizOpps Link to This Notice
(may not be valid after Archive Date)
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