REF: UAV-LRS-2000 // REV A
Surveillance UAV
2000 KM RANGE — TECHNICAL DRAWING PACKAGE
CLASS: CONCEPT DESIGN
PROP: JET / TURBOPROP
DATE: MAR 2026
01 — Orthographic Views
02 — Isometric View
03 — System Architecture
SIDE VIEW — PROFILE
10.8 m (OVERALL LENGTH)
0.9 m
NOSE/EO
EO/IR
WING
TURBOPROP ENGINE
/ SATCOM
PROP
V.STAB
H.STAB
TOP VIEW — PLAN
AILERON
AILERON
20 m WINGSPAN
WING SPAR (CFRP)
ENGINE
SATCOM
FRONT VIEW
20 m
~2° DIHEDRAL
KEY PARAMETERS
Range
2,000 km
Wingspan
18–22 m
Length
~10.8 m
MTOW
~1,500 kg
Engine
TPE331 940 shp
Cruise Alt
8–14 km
Speed
200–280 km/h
Endurance
20–30 hrs
Fuel Load
~850 L Jet-A
Payload
150–300 kg
ISOMETRIC — 3/4 UPPER PORT VIEW
NOSE / PITOT
EO/IR TURRET
TURBOPROP / NACELLE
SATCOM DOME
PORT WING — 20 m SPAN
VERT. STAB / RUDDER
AILERON
EXHAUST
APPROX. 5 m
NOT TO EXACT SCALE
SYSTEM ARCHITECTURE — UAV-LRS-2000
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
TURBOPROP
ENGINE + FADEC
TPE331 / 940 SHP
POWER
GEN 5–10 kVA
28VDC / 115VAC
FLIGHT SURFACES
SERVOS / EHA
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 RADAR
SIGINT / ELINT
LASER RGFDR
PAYLOAD CPU / GPU
FUEL SYSTEM
~850 L JET-A
WET WING + FUSELAGE
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 COVERAGE
LOS LINK
TERMINAL
UHF/L-BAND
~300 KM RANGE
ISR EXPLOITATION
VIDEO DISPLAY / RECORDING
FULL MOTION VIDEO (FMV)
TARGET GEOLOCATION / TAGGING
CRYPTO / COMSEC
AES-256 / TYPE-1 ENCRYPTION
KGV-SERIES OR EQUIV
GCS POWER
DIESEL GEN + UPS / 24-7 OPS
SATCOM C2 + ISR (Ku-BAND)
LOS LINK (UHF/L-BAND)
LEGEND
C2 / Avionics Data Bus
Payload / ISR Data
Power / Propulsion
RF Datalink (Air-Ground)
LOS RF Link
Avionics / Control Systems
Payload Systems
Propulsion / Power
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
DRAWING REV: A
SCALE: NOT TO EXACT SCALE — CONCEPT ILLUSTRATION
DATE: MAR 2026
CLASS: CONCEPT DESIGN / UNCLASSIFIED
HOVER CALLOUTS FOR COMPONENT DETAILS