SBIR/STTR Research Award

Soil Moisture Mapping sUAS

Award identifier 2f1b1041844d4253d3696bd473629d594912c43ee4c8a6c5aa52a7c886ed97a9Awarding agency National Aeronautics and Space Administration

Award amount

$874,751

Program and phase

SBIR · Phase II

Award year

2014

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BLACK SWIFT TECHNOLOGIES LLC
Proposal award date
2014-04-11
Contract end date
2017-01-10
UEI
C2J3K9NRE3L3
Solicitation number
Not reported
Topic code
S3.05

Research abstract

Black Swift Technologies proposes the continued development, testing, validation, and delivery of the SuperSwift small Unmanned Aircraft System (sUAS), with a highly capable passive microwave radiometer to provide full coverage soil moisture measurements over an area of 400 acres per flight. Tight integration of the sensor with the sUAS avionics and airframe will enable precise flight control for low altitude missions in the range of 15m-30m above ground level (AGL) required for the sensor to accurately map soil moisture down to ~5cm in depth at up to a 15m resolution. The teams strong working knowledge of the regulatory environment surrounding sUAS will be used to inform the development of the system and associated concept of operations. This will facilitate safe and legal operation in the national airspace following FAA approval. The continued SuperSwift system development will address the design issues identified in Phase I. The stock airframe utilized in the Phase I study, the Tempest, while well qualified for use in preliminary flight testing, created additional challenges for integration of the soil moisture measurement payload. Due to the requirements of the radiometer antenna the Tempest was modified during Phase I to accomplish initial flight testing, but had several challenges including external placement of the antenna, more complex manufacturing of the control linkages for the rudder and elevator, and a soil moisture electronics payload that is deeply integrated into the airframe and difficult to remove for testing and replacement. These requirements drove the team to design a modified fuselage to be built in Phase II that involves a modified removable nose cone to house the entire sensor payload and converts the propulsion to a twin engine design on the wings.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

24 SBIR/STTR records share this UEI (2013–2025). Reported award amounts total $7,731,683. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

National Aeronautics and Space Administration

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