DRAWING NO: UAV-PSH-001
CONFIG: PUSHER / INV-V TAIL
REV: A — CONCEPT DRAFT

PUSHER UAV

SINGLE PROP · INVERTED-V TAIL · 2000 KM RANGE
SCALE: NTS
DATE: MAR 2026
CLASS: CONCEPT
01 — THREE-VIEW ORTHO
02 — ISOMETRIC
03 — SYSTEM ARCHITECTURE
SIDE VIEW — PROFILE
AILERON PROP ~11 m OVERALL LENGTH 0.9 m PITOT/NOSE AVIONICS BAY WING SPAR ENGINE COWL INV-V FIN EO/IR
TOP VIEW — PLAN
18 m WINGSPAN PORT NAV (GRN) STBD NAV (RED) AILERON FLAP PUSHER ENGINE
FRONT VIEW
2° DIHEDRAL ~45° V ANGLE 18 m PORT STBD
DESIGN PARAMETERS
ConfigPusher / Inv-V
Range~2,000 km
Wingspan16–20 m
Length~11 m
MTOW600–900 kg
Engine100–200 hp
Fuel~700 L
Endurance24–36 hrs
Cruise120–180 km/h
Altitude5–8 km
Payload50–150 kg
ISOMETRIC — 3/4 UPPER PORT VIEW
PORT (GRN) PITOT / NOSE EO/IR TURRET PORT WING — 18 m SPAN PUSHER ENGINE / PROP INV-V FIN (RUDDEVATOR) AVIONICS / SATCOM ≈ 4.5 m NOT TO EXACT SCALE
SYSTEM ARCHITECTURE — UAV-PSH-001 (PUSHER / INV-V TAIL) AIRBORNE SEGMENT GROUND SEGMENT FLIGHT CONTROL COMPUTER (FCC) DUAL REDUNDANT NAV SUITE INS + GPS/GNSS ADC + RADAR ALT AIR DATA / TCAS ADS-B IN/OUT FLIGHT SURFACES AILERON / FLAP / RUDDEVATOR PUSHER ENGINE + FADEC 100–200 HP / PROP POWER BUS 28 VDC / ALTERNATOR AVIONICS DATA BUS MIL-STD-1553B + ARINC 429 COMMS SYSTEM Ku-BAND SATCOM UHF/L-BAND LOS VHF ATC / HF BACKUP AES-256 ENCRYPTED PAYLOAD SUITE EO/IR TURRET SAR / LIDAR (OPT) LASER RANGEFINDER SIGINT ANTENNA PAYLOAD CPU / GPU FUEL SYSTEM ~700 L JET-A / AvGas WET WING + FUSELAGE TANK VEHICLE HEALTH FDR / HUMS SENSOR FUSION GCS — OPERATOR STATIONS PILOT + PAYLOAD OPERATOR MISSION PLANNING SOFTWARE REAL-TIME VEHICLE CONTROL RUGGEDISED SHELTER / VEHICLE SATCOM TERMINAL Ku-BAND DISH GLOBAL BEYOND-LOS LOS LINK TERMINAL UHF/L-BAND ~250–300 KM ISR DATA EXPLOITATION FULL MOTION VIDEO + RECORDING TARGET GEO-LOCATION / TAGGING AI-ASSISTED OBJECT DETECTION (OPT) CRYPTO / COMSEC AES-256 / TYPE-1 ENCRYPTION MODULES GCS POWER SUPPLY DIESEL GENERATOR + UPS — 24/7 SATCOM C2 + ISR (Ku-BAND) LOS (UHF/L-BAND) LEGEND C2 / Avionics Bus Payload / ISR Data Power / Propulsion SATCOM RF Link LOS RF Link Avionics / Control Payload Systems Propulsion / Power PUSHER CONFIG ADVANTAGE: CLEAN NOSE = UNOBSTRUCTED SENSOR FOV · INV-V TAIL = FEWER PARTS · LOWER BUILD COST STANDARDS MIL-STD-1553B Data Bus STANAG 4586 GCS Interface STANAG 7023 ISR Data DO-178C SW Assurance ICAO Annex 2 Airspace MIL-STD-810H Environment ITAR / EAR Export Control
DRAWING NO: UAV-PSH-001 / REV A
CONFIG: PUSHER · INVERTED-V TAIL · SINGLE PROP SCALE: NOT TO EXACT SCALE DATE: MAR 2026 ● HOVER DOTS FOR COMPONENT DETAILS