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Innovative Ground Habitats for Lunar Operational Outpost (IGLOO)
Completed
TRL 3 (started at 2, targeting 3)
Description
NextGen Aeronautics, Inc. is proposing an alternate architecture for inflatable lunar habitats that takes advantage of inflatable beam technologies currently being used in various military, aerospace, and commercial applications. Current technology uses a fiber-reinforced elastomeric composite capable of containing high gas pressure, giving the beams the strength needed to form a robust structure that can withstand being buried by regolith for radiation/micrometeorite protection. NextGen's novel approach is to join multiple beams, forming a continuous cellular arched structures or a series of connected rings to form cylinders. Key advantages of this approach include: ability of structure to maintain strength and stiffness independent of pressure in habitable volume, double wall construction preventing puncture of internal/external wall, ability to isolate leaks in affected elements without compromising habitat pressure or structural integrity, possible use of water or other radiation absorbing material to fill beams, and relative ease of creating a rigid structure by filling the beams with foam. We will achieve TRL of 2 in Phase I and technology transition to TRL of 5 in Phase II. NextGen team's strength lies in related prior work, and with investigators who have an exceptional background in inflatable structures and low-stowed volume designs.
Benefits
Can be used for any application where low weight/volume is needed in transit, but large environmentally isolated habitable space is desired at location. This type of structure has seen previous applications even on Earth for Antarctic structures.
Future manned lunar missions with surface stays of more then a few days will require structures to provide habitation and support in addition to that provided by lunar landing vehicles. These structures must provide a pressurized environment with protection from thermal effects, radiation, dust, micrometeorites, moonquakes, and other hazards while being lightweight, easy to transport, and easy to deploy. Direct applications of the proposed effort pertain to these lunar or other missions where habitable space is needed.
Details
| Technology area | Entry, Descent, and Landing > Aeroassist and Atmospheric Entry > Hypersonic Decelerators |
| Program | Small Business Innovation Research/Small Business Tech Transfer (SBIR/STTR) |
| Lead organization | NextGen Aeronautics, Inc., Torrance, CA |
| Start date | 2010-01-29 |
| End date | 2010-07-29 |
Project contacts
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How to get involved
This is early/mid-stage (TRL 3) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.
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