SBIR/STTR Research Award

STTR Phase I: A Reliable and Efficient New Method for Satellite Attitude Control

Award identifier 7bd6afef311d4c0a93875d9553e4283890a846ea056a8eed68c1b93ea186f6e1Awarding agency National Science Foundation

Award amount

$274,993

Program and phase

STTR · Phase I

Award year

2024

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Award details

Awarding agency
National Science Foundation
Branch
Not reported
Recipient company
SAMARA AEROSPACE, INC.
Proposal award date
2024-02-01
Contract end date
2024-09-30
UEI
NAEPX9DPGKQ9
Solicitation number
NSF 23-515
Topic code
SP

Research abstract

This Small Business Technology Transfer (STTR) Phase I project offers significant changes to the conventional concept of spacecraft orientation control by providing increased agility, along with reduced mass, volume, and cost. These advantages open doors to new scientific and commercial opportunities. The project addresses the demanding needs of future space observatories and commercial spacecraft that require high agility systems, currently unachievable with existing attitude control solutions. Moreover, this system, as a more affordable 3-axis control option, is set to increase access to space for lower-budget missions, making space exploration more accessible than ever before. The systems application is envisioned to enable advances in sectors such as satellite-to-satellite communications, adding momentum to global digital connectivity initiatives. This STTR Phase I project seeks to develop a Multifunctional Structures for Attitude Control (MSAC) system and increase its efficiency and reliability, pushing it towards achieving readiness for flight demonstration. The project addresses the existing challenge of the system's fatigue strength and its compatibility with the harsh space environment, factors crucial for its commercial success and durability in its intended application. This project's aim is to design a flight-capable system, drawing on the insights from lab-scale tests and prototypes. It also seeks to simultaneously improve the system's mechanical and electrical design to elevate efficiency and reliability standards. Through this research method, the team anticipates a better understanding and eventual mitigation of potential failure modes, paving the way for the realization of a robust, space-ready prototype. The anticipated technical results from this endeavor have the potential to revolutionize the spacecraft attitude control market. This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

3 SBIR/STTR records share this UEI (2024–2025). Reported award amounts total $1,674,800. Reported amounts are not federal obligations.

Phases: Phase I, Phase II – Direct to Phase II

Agencies: Department of Defense, National Science Foundation, National Aeronautics and Space Administration

Agency intelligence

National Science Foundation

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