SBIR/STTR Research Award

Lightweight Structural Aerobrake for Orbital Positioning and Maneuvering

Award identifier 115b541da5368d95dccf102d62e1435f7631192f05f427da572d36f7f39ba404Awarding agency Department of Defense · Air Force

Award amount

$64,899

Program and phase

SBIR · Phase I

Award year

2001

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
AEROASTRO, INC.
Proposal award date
Not reported
Contract end date
Not reported
UEI
TCCYK6KJGN24
Solicitation number
Not reported
Topic code
Not reported

Research abstract

The ability to maneuver, change orbits, and rapidly deploy spacecraft is a key requirement for the space user community. However, large and bulky propulsion systems with a significant mass of fuel on board often limit the maneuverability and capabilitiesof space vehicles. AeroAstro is developing aerobraking concepts and structures that use the Earth's atmosphere for braking and steering, significantly reducing the amount of propellant and even the type of propulsion systems required on spacecraft. Verylightweight aerobraking structures can enable significant reduction in mass coupled with an increase in capability.Using aerobraking, AeroAstro is developing with commercial funding the Small Payload ORbit Transfer (SPORTT) system to enable small payloads to use low-cost secondary launch opportunities and still reach custom orbits. A lightweight aerobrake structuraldesign is key to the SPORT concept. To fit within constrained volumes, aerobraking structural members must be tightly packaged and lightweight. Structural booms must deploy to approximately ten times their length to produce a seventy-fold increase inprofile area. AeroAstro proposes to investigate various applications and structural technologies for the aerobrake design.TThe use of aerobraking provides spacecraft and vehicles like SPORT with a much greater orbit transfer capability than that achievable with direct propulsion. Aerobraking reduces the ?V requirement for a GTO to LEO orbit transfer from a costly 2,340 m/sdown to an affordable 378 m/s, an amazing 84% reduction in ?V requirement. While the GTO to LEO case is extreme, other transfer missions, such as GEO to LEO and LEO to Intercept, each reveal a 50% savings in the ?V requirement. This will result in amassive reduction in launch costs for small satellites.The aerobraking technology payoff is significant, with commercial and government utility forseen not only for the SPORT vehicle, but also in a variety of other applications. Potential applications for the aerobraking technology include population ofmicrosatellite constellations, situational pre-positioning, and space asset resupply.There are numerous potential customers, both government and commercial, for the technology that AeroAstro is proposing to develop. The first customer for this aerobraking technology will likely be a customer for AeroAstro's SPORT vehicle. A commercialcustomer is already funding a feasibility study for the first SPORT, which could be launched in 2003-2004.

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

51 SBIR/STTR records share this UEI (1992–2008). Reported award amounts total $21,736,033. 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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