SBIR/STTR Research Award

Precision-Angle Tension-Stabilized (PATS) Anti-Personnel Obstacle Breaching System (APOBS)

Award identifier afbf8bacf2b9e3ff5d773b2657b3fb0b94b9a3267d55d0eed8be74d3603edd2aAwarding agency Department of Defense · Navy

Award amount

$139,855

Program and phase

SBIR · Phase I

Award year

2023

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
PROTECTION ENGINEERING CONSULTANTS LLC
Proposal award date
2023-06-14
Contract end date
2024-04-12
UEI
KWVLNBS42RD8
Solicitation number
23.1
Topic code
N231-001

Research abstract

The current Anti-Personnel Obstacle Breaching System (APOBS) consists of grenades, equally spaced on a fabric reinforced detonating cord over-braided in a polyester support structure. The APOBS kit contains 45-meters of line charge, a rocket motor to propel the system over the target, and a drogue chute to ensure straight-line deployment. Currently the launch rod for the APOBS rocket is installed at a fixed angle. During set-up on uneven or hilly terrain, Marines are trained to improvise backpack supports to adjust the angle of the launch rod. This SBIR topic would identify a lightweight engineering design solution and tool to identify and set an optimal launch angle for APOBS rocket motor deployment. The optimal deployment of the APOBS grenades is a straight line. Due to rocket motor thrust, drogue chute loads, impulse drag from the rear backpack assembly, environmental conditions, or some unknown factor during deployment, the system sometimes deploys with a transverse wave along the detonating cord. This transverse wave can result in arc, u-shape or loops forming along the detonation cord. These non-straight geometric arrangements of the APOBS after deployment may result in unexploded grenades as the grenades detonate from the rear and front fuzes to the center connector. The purpose of this SBIR topic is to modify the APOBS system to (1) allow variable launch angles that can be optimized based upon terrain, and (2) resolve the shape instability issues that result in non-linear deployments.  The Phase I technical objectives will include: Design an adjustable angle launch rod mechanism. Determine the root cause of the transverse wave instabilities. Design a tension-stabilizing solution for the transverse wave instability. Demonstrate the feasibility of design changes in terms of function, manufacturability, packaging, and ease of use. Develop detailed plan for Phase II effort.

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

36 SBIR/STTR records share this UEI (2006–2025). Reported award amounts total $13,338,282. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, Department of Transportation, Department of Energy

Agency intelligence

Department of Defense

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