This Government Contract opportunity from Department Of Defense was posted on May 15, 2026. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

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Rocket Motor Design & Engineering Services

Closed

Federal

Submission Closed06/15/2026, 09:00:00 PM UTC

Contract Overview

Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

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NAICS: 541330

New

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in 10 days

DEADLINE

in 10 days

AI Contract Overview

The contract involves the preliminary and detailed design of a solid-propellant ducted rocket motor, encompassing computational modeling as well as thermal and structural analysis. A key component of the task includes integrating the design with Government-owned technical data packages. The work is classified as a subcontract under the Naval Air Systems Command within the Department of Defense, focusing on professional engineering services categorized under NAICS code 541330. The place of performance is designated as St James, with a response deadline set for mid-June 2026. This engagement emphasizes advanced technical design and engineering activities supporting defense-related rocket motor development.

General Info

Design and analysis of solid-propellant ducted rocket motor subcontract, St James, deadline June 2026.

Agency

Department Of Defense → Naval Air Systems Command

NAICS

541330 - Engineering ServicesView NAICS

Place of Performance

St James, MD, 20670, USA

Set-Aside

NONE

Documents

(0)

No documents available

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Timeline

PhaseClosed

PostedMay 15

subcontract

Response DeadlineJun 15

Deadline has passed

Submission Closed

06/15/2026, 09:00:00 PM UTC

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Organization & Contact Information

AgencyDepartment Of Defense → Naval Air Systems Command

ContactsNo contacts available

OfficeN/A

Organization / Agency

Department Of Defense → Naval Air Systems Command

Office AddressN/A

ContactsNo contact information available

Full Description

Preliminary and detailed design of a solid-propellant ducted rocket motor including computational modeling, thermal/structural analysis, and integration with Government-owned TDP.