2026-11-06 Attachment C - System Summarization.pptx

Attachment C – (Company Name / Name of System)

PHYSICAL DESCRIPTION

Size/Dimensions:

Weight:

Docking Station / Enclosure Dimensions and Weight:

Aircraft Power Source:

Docking Power Source:

Payload Configuration:

Dock System Graphic sUAS Graphic

Day Camera

Target 38.889466, -77.035243

Type: Size: Total Cost: $ Dock: $ Airframe: $ Sensor Pkg: EO: $ IR: $ Production: x days / x units per month

AUTONOMY, SOFTWARE, & INTEGRATION

Autonomy & AI Capabilities:

C2 and Video Integration:

Data Security & Logging:

SUITABILITY/READINESS

Number of Operators Required:

Turnaround / Recharge Time:

Regulatory & Airworthiness Status:

Current Federal Aviation Administration (FAA) approvals:

Recharge Time:

Technological Readiness Level (TRL):

Manufacturing Readiness Level (MRL):

PERFORMANCE

Maximum Flight Endurance / Hover Time:

Operational Radius / Control Range:

Maximum Cruise and Dash Speeds.

Weather & Environmental Tolerances:

Autonomous Launch & Recovery Limits:

Instructions/Guidance for filling out Attachment C - 1 Page Summary

The purpose of the 1 page summary is to provide an easy overall reference for the Dock and sUAS platform that your company has developed. This summary should provide an overview of the size, cost, and capabilities of the system.

Provide a separate Attachment C for each system proposed.

Company Name / Platform Name / Size / Cost / Production.

Size: Nano: Gross takeoff weight < 250 grams (g); Micro: ≥ 250 g and ≤ 2000 g; Very Small: > 2000 g and ≤ 9.1 g; Small: > 9.1 and ≤ 25 kilogram.

Cost – Total cost and cost of airframe and sensor packages.

Manufacturing Lead Time – Days after contract award for delivery of 1st unit and number of units per month thereafter.

Platform (Aircraft) Description:

General physical description of system: Baseline with Sensors / Maximum gross takeoff weight / Maximum Payload weight - Power source and weight Radiofrequency spectrum information: Does it operate in unlicensed or is there equipment certification and frequency assignments (licenses) for CONUS use. For licensed frequencies, list frequencies for control link, ATC radios, transponders, detect and avoid systems, and navigation systems.

Shipping/transport weight: Include packaging/pelican case configurations / power/battery weights. What comes with the airframes?

Platform Performance: General performance characteristics of airframe with propulsion system. Noise levels if available. Endurance of system under various conditions. Provide motor/propeller characteristics (ie, volts, prop size, Kv, RPM). Power source/battery characteristics. List types of sensors that can be used (more detail on EO/IR in next boxes).

Sensor - EO Performance: Performance at 400ft and 1200 ft elevation in terms of detection/identification of human/animal/conveyance in both day and darkness conditions. Provide characteristics of day camera, gimbal and stabilization. Low light as well as optical zoom/Field of view options. Digital zoom? Sensor size and recording capability.

Sensor - IR Performance: Performance at 400ft and 1200 ft elevation in terms of detection/identification of human/animal/conveyance in both day and darkness conditions. Provide characteristics of IR camera capabilities including gimbal and stabilization. Field of view options. Sensor type and size and recording capability.

Unique Capabilities and/or Future Capabilities

- Integrated with Latice

- Encrypted radio/Communication relay capability

- Object avoidance

- Video analytics

- Object Tracking and Following

- Cursor on Target

- ADS-B transponders

- Communications relay capabilities

- Easy integration with other sensors image1.jpeg