SBIR/STTR Research Award

Compact, Lightweight Bolt-on Deorbit Device for Spacecraft

Award identifier 16c0ccb3e8b19aeff0e9e243495e1b1056fc5a68945b4d2b6d6ccab2717af0f8Awarding agency National Aeronautics and Space Administration

Award amount

$124,899

Program and phase

SBIR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
L'GARDE, INC.
Proposal award date
2019-08-19
Contract end date
2020-02-18
UEI
LEUWTPVHDXA8
Solicitation number
SBIR_19_P1
Topic code
Z8

Research abstract

The space environment around the earth is now littered with both functioning and non-functioning satellites.nbsp; This is over and above the man-made debris generated as a result of launching these space objects and their density is increasing exponentially with time.nbsp; If nothing is done about this, the earth will eventually have its own Saturn ring if not a spherical shell of orbiting objects and debris. There is definitely a pressing need for an inexpensive and reliable method of de-orbiting satellites after their mission life has ended. We propose to carryout a for a passively deployable, lightweight, low-compaction ratio bolt-on de-orbit device for satellites.nbsp; The de-orbiter is packaged intonbsp;a small bolt-on canister that gets attached to the spacecraft.nbsp; It stays in the packaged configuration until the end of the satellite mission at which time it is activated deploying the de-orbit element out of its canister, increasing the spacecraft drag area against the atmosphere.nbsp; For high low-earth orbit starting altitudes where the atmospheric density is extremely low, the de-orbiter drag sail is made to work like a solar sail capitalizing on the solar radiation pressure but in this case to decrease the satellites energy thereby lowering its altitude over time. It is pointed out that using this solar-sailing approach has practically unlimited delta v capability.nbsp;The innovation in the proposed de-orbiter design is the use of a proprietary shape memory composite material for the structural elements of the de-orbiter.nbsp; It is foldable and packageable into a small stowed volume and deployment is passively achieved by simply releasing the stored strain energy in the packaged configuration.nbsp; Tests and measurements performed in the laboratory show that the material formulation we use achieves deployment to the memorized configuration even after the material has been in the folded state for years. When the solar sail mode is used, itnbsp;can be used to extend the satellite lifetime.

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

67 SBIR/STTR records share this UEI (1983–2025). Reported award amounts total $21,901,140. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy, Department of Commerce

Agency intelligence

National Aeronautics and Space Administration

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