SBIR/STTR Research Award

Bi-Fold Fan DragSail with Surface Area Modulation Capability

Award identifier 928f190f46e765cefd347324f51fae6ceea5c03e1b0bc38719c10c33b9eddbc3Awarding agency National Aeronautics and Space Administration

Award amount

$124,997

Program and phase

SBIR · Phase I

Award year

2020

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
NEXOLVE HOLDING CO LLC
Proposal award date
2020-08-12
Contract end date
2021-03-01
UEI
YEQZGZRT2L87
Solicitation number
SBIR_20_P1
Topic code
Z8

Research abstract

A new passive reentry system is proposed for deorbiting spacecraft from low earth orbit (LEO).nbsp; The proposed DragSail system is based upon a restowable and redeployable concept that allows for increase or decrease of surface area thus modulating aerodynamic drag of the system.nbsp; Modulation of the drag will allow the system to guide small spacecraft to specific locations at the Von Karman altitude, which is necessary for precision reentry targeting.nbsp; The primary objective of this DragSail design is to deorbit small spacecraft from LEO altitudes in 25 years or less using a modular DragSail system with minimal weight and stowage volume.nbsp; The proposed DragSail system is based on NeXolve-developed lightweight solar sail and deployment system technologies.nbsp; The concept design consists of ultralightweight polyimide thin-film material that is attached to a deployable boom structure to create a flexible DragSail system with shape morphing capability.nbsp; A key feature of this DragSail system is its ability to deploy as a 2-D structure and then shape morph into a 3-D structure that allows drag in all orbital orientations.nbsp; Another attractive feature of the design is that the system is a self-contained unit that can be attached to many different types of CubeSats and small satellites.The DragSail system proposed herein is a scalable system that will allow CubeSats and small satellites up to 200 kg to deorbit from altitudes between approximately 700-1100 km in 25 years or less with the potential for similar results up to 2,000 km.nbsp; This innovative restowable, redeployable 3-D shape morphing membrane system is capable of increasing cross-sectional area impinging in all positions along an orbital path.nbsp; Partial deployment or partial morphing will enable changes in orbital decay rates allowing for collision avoidance as well as targeted atmospheric re-entry.nbsp; This 3D shape morphing capability is a significant advantage over flat (2-D) constructions.nbsp;

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

11 SBIR/STTR records share this UEI (2018–2024). Reported award amounts total $4,474,243. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Commerce

Agency intelligence

National Aeronautics and Space Administration

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