SBIR/STTR Research Award

A Modular High Power Solar Array for NanoSats

Award identifier ac4b565ab0b787bc7afa792c3ef259348eb0700d9e3bbd568e7b082208544c2bAwarding agency Department of Defense · Air Force

Award amount

$749,942

Program and phase

SBIR · Phase II

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
M.M.A. DESIGN LLC
Proposal award date
2012-06-04
Contract end date
Not reported
UEI
HJGNEC99TWV5
Solicitation number
2010.3
Topic code
AF103-089

Research abstract

ABSTRACT: With increased focus on development of highly capable NanoSat spacecraft and missions, innovations in system design and architecture yielding high performance, modular and multi-function systems will enhance Air Force mission utility, capability and flexibility. An area of considerable development opportunity enabling Air Force NanoSat missions is to increase available continuous power significantly, to lower costs and to further leverage this capability to effectively de-orbit the spacecraft at end-of-life. MMA Design proposes to significantly advance the state-of-the-art in NanoSat power systems by completing development and delivering our Enhanced High Watts per Kilogram (E-HaWK) solar power system with a modular and scalable architecture. It consists of innovative deployable solar arrays combined with a sun tracking gimbal assembly that is initially optimized for a 3U but readily adaptable to a 6U Bus configuration. The significance to the Air Force of our innovative solution is that it allows the spacecraft to maintain high power while freeing the mission instruments to track an area of interest, thus improving mission utility, flexibility and capability. The E-HaWK innovations further demonstrate MMA"s NanoSat modular solar power architecture for providing a range of mission power options and leverages from our core solar power technologies. BENEFIT: 1. Space Situational Awareness two axis sun tracking allows the S/C to maintain high continuous power while simultaneously freeing the mission instruments to track an AOI, thus improving mission capability, flexibility and utility. 2. Mission ISR data and quality can increase with increases in power capabilities, power tracking and performance. 3. Maximizing the utility of the available volume by combining the functions of solar power and de-orbiting into one robust deployable system. 4. Rapid development and maturation of innovative spacecraft power and bus technologies leading to low cost solutions that are adaptable and scalable to other AFRL applications. 5. Advancement of key deployable and steerable solar array technologies to overcome current NanoSat spacecraft and mission limitations. 6. A highly modular and scalable system design. 7. A low mass/volume and high performance 3U bus system to maximize the mass/volume available for payloads. 8. De-orbit capability ensures reduction in future space debris and available orbital slots. 9. The MMA team offers Air Force high innovative content for revolutionizing NanoSat technologies with high risk/reward payoffs. Air Force can leverage our small company performance advantages in the areas of technical, schedule and cost.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

20 SBIR/STTR records share this UEI (2009–2023). Reported award amounts total $11,235,796. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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