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This Government Contract opportunity from National Aeronautics And Space Administration was posted on April 30, 2026. The submission period has ended. Browse the details below for market research, or find similar active opportunities.

Structural Analysis and Frequency Modeling

Closed
Federal

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The contract involves performing modal and finite element analysis focused on ensuring that the structural frequencies of a CubeSat avoid resonance or coupling with the dynamics of the Space Launch System (SLS) vehicle. The analysis must confirm that frequency thresholds are met across all axes to maintain structural integrity and compatibility during launch. The work is classified under NAICS code 541380 and is a subcontract opportunity issued by NASA's Marshall Space Flight Center. The solicitation was posted on April 30, 2026, with a response deadline of May 31, 2026, and is to be performed in Huntsville. The primary objective is to conduct detailed frequency modeling and structural analysis to support the safe integration of the CubeSat with the SLS vehicle, helping to mitigate risks related to vibrational interactions during the launch vehicle’s operation. This contract is critical to ensuring mission success by addressing structural dynamics and compatibility concerns early in the CubeSat development process.

General Info

Perform modal and finite element analysis ensuring CubeSat structural frequencies avoid SLS resonance.

Agency

National Aeronautics And Space Administration → NASA Marshall Space Flight Center

NAICS

541380 - Testing Laboratories and ServicesView NAICS

Place of Performance

Huntsville, AL, 35812, USA

Set-Aside

NONE

Documents

(0)

No documents available

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Timeline

PhaseClosed
Posted

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Response Deadline

Deadline has passed

Submission Closed

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Organization & Contact Information

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AgencyNational Aeronautics And Space Administration → NASA Marshall Space Flight Center
ContactsNo contacts available
OfficeN/A
Organization / Agency
National Aeronautics And Space Administration → NASA Marshall Space Flight Center
Office AddressN/A
ContactsNo contact information available

Full Description

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Perform modal and finite element analysis to ensure CubeSat structural frequencies avoid coupling with SLS vehicle dynamics, meeting thresholds in all axes.