Login
Login
Register
Complete Your Profile
Change Password
Request a Password Reset
Download Documents
Download Documents
Get Help to Participate in This Tender
Change Password
For better security, update the account password.
DEPT OF DEFENSE | DEPT OF THE ARMY has floated a tender for seat stabilization rocket motors mt32 or md98. The project location is USA and the tender is closing on 03 Feb 2026. The tender notice number is W519TC-26NB017-SS, while the TOT Ref Number is 134059182. Bidders can have further information about the Tender and can request the complete Tender document by Registering on the site.
Procurement Summary
Country: USA
Summary: seat stabilization rocket motors mt32 or md98
Deadline: 03 Feb 2026
Posting Date: 21 Jan 2026
Other Information
Notice Type: Tender
TOT Ref.No.: 134059182
Document Ref. No.: W519TC-26NB017-SS
Financier: Self Financed
Purchaser Ownership: Public
Tender Value: Refer Document
Purchaser's Detail
Name: Login to see tender_details
Address: Login to see tender_details
Email: Login to see tender_details
Login to see detailsTender Details
The U.S. Army Contracting Command, Rock Island, on behalf of PM-CCS (Project Manager, Close Combat Systems), is issuing a sources sought notice to identify capable sources for the production and delivery of the following items.
Item NSN Part Number DODIC
Seat Stabilization Rocket Motor (SSRM) 1377-01-255-1650 3205AS103 MT32
Seat Stabilization Rocket Motor (SSRM) 1377-01-318-1830 1340-1 MD98
Specifications:
Seat Stabilization Rocket Motor (SSRM)
Specifications: Douglas Aircraft Specification DACA114301
Revision: U
Revision Date: 28 Aug 1989
OR
Seat Stabilization Rocket Motor (SSRM)
Specifications: MIL-DTL-85097 (OS)
Revision: E
Revision Date: 2 Jul 2001
ITEM DESCRIPTIONS: This device provides power to stabilize the ejection seat during emergency aircrew escape. It counteracts forces, which tend to pitch the seat during rocket motor burn of the rocket catapult.
No ozone depleting agents are used in the production of this item. If contractors propose an alternate data package, the U.S. Government will require the use of the PVU-1/A primers (provided as GFP).
The article consists of a mechanically fired rocket motor having twin combustion chambers along a common axis on either side of a nozzle perpendicular to this axis. Ball bearing supports on either side of the nozzle allow rotation of the motor during firing this providing for controlled direction of thrust.
Envelope: The rocket motor shall conform to the dimensions shown in the TDP.
Mounting Provisions: The rocket motor is to be provided with two anti-friction bearing journals located on either side of the nozzle as shown in Figure 1 of the TDP. These journals provide for the mounting of two bearings to be used in support of the motor.
Please see the attached TDP to adhere to all the figures and specifications located within.
CRITICAL PROCESSES/SKILLS: The manufacture of this item requires skills, which include, but are not limited to:
Radiogr...
Notice ID: w519tc-26nb017-ss
Department/Ind. Agency: dept of defense
Sub-tier: dept of the army
Office: w6qk acc-ri
Product Service Code: 1377 - cartridge and propellant actuated devices and components
NAICS Code: 333998 - All Other Miscellaneous General Purpose Machinery Manufacturing
Inactive Dates: feb 18, 2026
Inactive Policy: 15 days after response date
Documents
Procurement Documents for USA
Access a comprehensive library of standard procurement documents specific to USA. Here, you'll find all the essential forms, guidelines, and templates required for tender applications and submissions in USA
Want To Bid in This Tender?
Get Local Agent Support in USA and 60 More Countries.
View Tenders By
Sign in with Google