Small Business Innovation Research/Small Business Tech Transfer
Titan Montgolfiere Buoyancy Modulation System
Project Description
Titan is ideally suited for balloon exploration due to its low gravity and dense atmosphere. Current NASA mission architectures baseline Montgolfiere balloon systems, which use waste heat from a radioisotope power system to heat balloon interior gases to provide buoyancy. A disadvantage of this approach is that the balloon is unable to make rapid changes in altitude which limits system utility. The feasibility of adding a rapid buoyancy modulation subsystem which uses chemical reactions to provide high heat input to balloon interior gases will be assessed in the proposed effort. Several concepts, including the baseline, will be traded on the basis of heat release capability and mass/volume efficiency in the context of proposed mission requirements, a concept will be selected and refined, and a lab scale demonstration of the reaction mechanism will be conducted in a relevant environment. Aurora's baseline Titan Montgolfiere Buoyancy Modulation System (BMS) concept uses a catalytically piloted burner, which combusts onboard stored oxygen with atmospheric gas, to provide rapid heat input an order of magnitude higher than the balloon's primary heat source. This system is scalable, lightweight, consumes minimal electrical energy, and is capable of providing altitude changes of approximately 200 m in under 60 s.
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Anticipated Benefits
Aurora believes that proposed baseline BMS concept is marketable in terrestrial applications where extremely high altitude exploration is valuable. Examples include long duration weather balloons that may be used to survey the climate at multiple altitudes during their deployment, and high altitude intelligence, surveillance, reconnaissance (ISR) aircraft propulsion systems. Potential customers may include the Defense Advanced Research Projects Agency (DARPA), the Air Force, and the Navy. The concept may also be of use to other agencies around the world, such as the European Space Agency (ESA), planning exploratory mission to Titan.
At its core, the proposed baseline Titan Montgolfiere BMS concept is a highly stable combustion system for use in adverse environments. In the literal sense the concept is inherently linked to Titan, and as such Aurora believes that the BMS could find application as a primary, or secondary, high output heat source on a wide range of potential exploratory platforms on the moon. For instance, the system could be used on other aerial systems, such as winged aircraft or aerobots, and ground based architectures, such as rovers or lake landers, for primary propulsion or power generation. In a more general sense, the combustor and catalytic pre-burner technology developed in the Phase I effort may also be applicable to terrestrial systems, such as high altitude aircraft propulsion or Montgolfiere burners. As the BMS concept and technology are matured Aurora believes that more commercial and science applications of the technology will develop. More »
At its core, the proposed baseline Titan Montgolfiere BMS concept is a highly stable combustion system for use in adverse environments. In the literal sense the concept is inherently linked to Titan, and as such Aurora believes that the BMS could find application as a primary, or secondary, high output heat source on a wide range of potential exploratory platforms on the moon. For instance, the system could be used on other aerial systems, such as winged aircraft or aerobots, and ground based architectures, such as rovers or lake landers, for primary propulsion or power generation. In a more general sense, the combustor and catalytic pre-burner technology developed in the Phase I effort may also be applicable to terrestrial systems, such as high altitude aircraft propulsion or Montgolfiere burners. As the BMS concept and technology are matured Aurora believes that more commercial and science applications of the technology will develop. More »
Primary U.S. Work Locations and Key Partners
| Organizations Performing Work | Role | Type | Location |
|---|---|---|---|
| Aurora Flight Sciences Corporation | Lead Organization | Industry | Cambridge, Massachusetts |
| Jet Propulsion Laboratory (JPL) | Supporting Organization | FFRDC/UARC | Pasadena, California |
Primary U.S. Work Locations
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California
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Massachusetts
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This is a historic project that was completed before the creation of TechPort on October 1, 2012. Available data has been included. This record may contain less data than currently active projects.