Attachment 2_Specifications_1232SA26Q0909.pdf
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- Attached to
- Unmanned Aerial Vehicle
- Solicitation number
- 1232SA26Q0909
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Unmanned Aerial Vehicle (UAV) Technical Specifications Summary
This document establishes minimum technical specifications for a professional-grade, NDAA-compliant Unmanned Aerial Vehicle system intended for federal U.S. Government operations. The required system comprises one multirotor quadcopter airframe with a 4.5–6.0 kg maximum takeoff weight, minimum 28-minute flight endurance with payload, and IP43 environmental sealing rated for –4°F to 122°F operating temperatures. The airframe must feature triple-redundant IMU architecture, dual-band GNSS (GPS, GLONASS, Galileo, BeiDou) with RTK-enabled flight controller, secure command-and-control link, and minimum 3+ mile line-of-sight control range. All components must be NDAA-compliant with no People's Republic of China-restricted parts.
The payload requirement specifies a LR1-class stabilized imaging system with 3-axis gimbal stabilization, minimum 20 MP still imagery capability, 4K video at 30 fps or higher, and maximum 500 g weight. The power system includes six intelligent lithium-ion or lithium-polymer flight batteries (98–100 Wh capacity, TSA-compliant, 200+ cycle life) with hot-swap capability and an SL8-class multi-bay fast-charging system providing rapid charge, battery health diagnostics, and thermal protection. An RTK GNSS ground reference station must deliver centimeter-level horizontal and vertical accuracy with real-time corrections to the aircraft, full flight controller integration, long-range correction link capability, and native RTK corrections without third-party receivers. Deliverables include the airframe, LR1 payload, six batteries, charger, RTK ground station, remote controller, protective carrying case, spare propellers, and complete documentation (manuals, safety sheets, maintenance guides). Mission-planning software with waypoint, grid, and corridor mapping plus secure local-only data storage options must be included.
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| File | Type | Posted |
|---|---|---|
| 1449_1232SA26Q0909.pdf | ||
| Attachment 1 - Solicitation Terms and Conditions_1232SA26Q0909.pdf |
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Unmanned Aerial Vehicle (UAV) Technical Specifications
SCOPE
This document defines the minimum technical requirements for a professional-grade, NDAA-compliant Unmanned Aerial Vehicle (UAV) suitable for federal U.S. Government operations. The system must include:
• One (1) multirotor quadcopter UAV airframe
• One (1) LR1-class stabilized imaging payload
• Six (6) intelligent flight batteries
• One (1) SL8-class multi-bay fast-charging system
• One (1) RTK-enabled ground reference station providing centimeter-level horizontal and vertical accuracy
• All required accessories for safe and effective operation
SYSTEM REQUIREMENTS
The UAV must meet or exceed the following:
• Multirotor configuration with foldable or compact transport design
• Maximum takeoff weight (MTOW): 4.5–6.0 kg
• Flight endurance: Minimum 28 minutes with LR1 Payload (included below, see Payload)
• Ingress protection: Minimum IP43 or equivalent environmental sealing
• Operating temperature range: –4°F to 122°F (–20°C to 50°C)
• NDAA-compliant components (no PRC-restricted parts)
AVIONICS AND NAVIGATION
The UAV must include:
• Triple-redundant IMU architecture
• Dual-band GNSS (GPS, GLONASS, Galileo, BeiDou)
• RTK-enabled flight controller compatible with external ground station
• Secure command-and-control link
• Minimum control range: 3+ miles (LOS)
LR1-CLASS PAYLOAD
The UAV must include a stabilized imaging payload meeting or exceeding the following:
• 3-axis gimbal stabilization
• High-resolution RGB sensor suitable for mapping, inspection, and documentation
• Global shutter or equivalent low-distortion capture
• Minimum 20 MP still imagery
• 4K video capture at 30 fps or higher
• Payload weight: ≤ 500 g
• Full integration with aircraft flight controller and mission software
POWER SYSTEM REQUIREMENTS (Batteries)
The system must include six (6) intelligent flight batteries meeting:
• High-energy-density Li-ion or Li-poly chemistry
• Smart battery management system (BMS) with cell balancing
• Minimum capacity: 98–100 Wh per battery (TSA-compliant)
• Hot-swap capability
• Cycle life: ≥ 200 cycles
BATTERY CHARGER
The charging system must:
• Provide rapid-charge capability
• Provide battery health diagnostics
• Include over-voltage, over-current, and thermal protection
RTK GROUND STATION REQUIREMENTS
The UAV package must include an RTK GNSS ground reference station that provides:
• Centimeter location accuracy horizontally and vertically
• Must support real-time corrections to the aircraft via radio link
Compatibility
• Fully integrated with the aircraft’s flight controller
• Must support long-range correction link
• Must allow base-rover pairing without third-party hardware
• Support native RTK corrections without third-party receivers
Hardware Requirements
• Multi-constellation GNSS receiver
SOFTWARE REQUIREMENTS
The UAV ecosystem must include:
• Mission-planning software with waypoint, grid, and corridor mapping
• Secure data handling with local-only storage options
DELIVERABLES
The vendor must provide (including the specs mentioned above):
• UAV airframe
• LR1-class payload
• Six (6) flight batteries
• Battery charger
• RTK GNSS ground station
• Remote controller
• Protective carrying case
• Spare propellers
• Documentation (manuals, safety sheets, maintenance guides)
File details come from the government source that posted it. Updated .