ENGINEERING DATASHEET

System Specifications

Comprehensive hardware, sensor, and RF subsystem tolerances for the Starling 2 Max aerial vehicle integrated with Theonic Labs Needle copilot and Aeroscan survey telemetry.

01 // EMBEDDED COMPUTE & AVIONICSQUALCOMM QRB5165
Processor CoreQualcomm QRB5165 8-Core Kryo 585 CPU (up to 2.84 GHz)
Neural Processing (NPU)Hexagon 698 DSP with Vector eXtensions (15 TOPS)
System Memory8GB LPDDR5 PoP RAM, 128GB UFS 3.1 Onboard Flash
Autopilot StackPX4 Autopilot (Offboard Mode over high-speed MAVLink)
Operating SystemModalAI VOXL SDK / Linux Kernel 4.19 aarch64 (Ubuntu base)
IPC ArchitectureZero-Copy Modal Pipe Architecture (MPA) POSIX Pipes
02 // SPATIAL LOCALIZATION & GPS-DENIED NAVIGATIONSUB-MILLIMETER QVIO
Odometry EngineqVIO (Qualcomm Visual-Inertial Odometry) + EKF2 Fusion
Optical Tracking SensorsDual Monochrome Global Shutter Cameras (120° FOV)
IMU Sensor SuiteDual redundant 6-DOF IMUs (TDK InvenSense ICM-42688)
Vertical Height ReferenceDownward Infrared Time-of-Flight (ToF) Rangefinder (0.1–8m)
Pose Update Rate30 Hz Visual Updates fused with 1000 Hz IMU Integration
Drift Tolerance< 0.1% cumulative position drift per 100m translation
03 // RF INTERCEPTION & WI-FI SPECTRUM FRONTENDTRI-BAND MT7921AU
Supported Frequency Bands2.4 GHz, 5.0 GHz, and 6.0 GHz (Wi-Fi 6, 6E, and Wi-Fi 7)
Capture ModesActive probe scanning + passive beacon sniffing (nl80211)
Channel Widths20, 40, 80, 160, and 320 MHz channel allocations
Sensitivity & Dynamic Range-95 dBm to -20 dBm RSSI measurement range
Sampling RateContinuous sweep (1.0–2.5s full band cycle at hover nodes)
04 // AIRFRAME & OPERATIONAL ENVELOPESTARLING 2 MAX AIRFRAME
All-Up Flight Weight~540g (including RF telemetry payload & battery)
Flight Endurance14–18 minutes per rapid-swap LiPo battery cartridge
Survey Speed0.5 m/s to 1.5 m/s autonomous programmed speed
Operating Temperature0°C to +45°C indoor warehouse / industrial envelope
NDAA / Legal Compliance100% NDAA Section 889 compliant components & US/UK IP origin