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Space Vehicle Bus & Architecture Design

Active
Federal

Contract Overview

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This subcontract involves the design and development of a payload-agnostic space vehicle bus and architecture intended for prime contractors supporting US Space Force Space Systems Command projects. The primary objective is to engineer a vehicle capable of hosting various vendor payloads and government furnished equipment while maintaining strict compliance with the Small Launch Interface Spec and Port Launch Users Guide for operations within low Earth orbit and medium Earth orbit regimes. The scope of work includes the delivery of comprehensive space vehicle architecture designs, model-based systems engineering files, and a fully integrated bus. This effort is managed under the Department of Defense through the Space Development Agency and Combat Power organization, with performance centered in the 90245 zip code area.

General Info

Subcontract for designing a payload-agnostic space vehicle bus for US Space Force projects.

Agency

Department Of Defense → FA8819 Sda And Combat Power Szk-LaView Agency

NAICS

336414 - Guided Missile and Space Vehicle ManufacturingView NAICS

Place of Performance

CA, 90245, USA

Set-Aside

NONE

Documents

This scope was carved out of SYD89-26-RPO-RLSV.

The full solicitation package (1 document), including the RFP, is on the prime solicitation, not on this scope.

View the prime solicitation

Rendezvous, Proximity Operations (RPO) Threat Response (RTR) VICTUS Responsive Launch Space Vehicle (SV)

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Organization & Contact Information

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AgencyDepartment Of Defense → FA8819 Sda And Combat Power Szk-La
ContactsNo contacts available
OfficeN/A
Organization / Agency
Department Of Defense → FA8819 Sda And Combat Power Szk-La
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Office AddressN/A
ContactsNo contact information available

Full Description

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Designs and develops a payload-agnostic space vehicle (SV) bus and architecture for prime contractors on US Space Force Space Systems Command projects. Engineers the vehicle to host diverse vendor payloads and GFE while ensuring compliance with Small Launch Interface Spec (SLIS) and Port Launch Users Guide (PLUG) for LEO and MEO orbital regimes. Delivers space vehicle architecture design, MBSE files, and an integrated bus.

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