Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
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Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
Quality 1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability factory
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1.5-ton Payload Hybrid USTOL Aircraft with 1200 km Range and 100-meter Takeoff Capability

Product Details


Maximum Takeoff Weight: 4,500 Kg Rated Payload: 1,500 Kg
Cruising Speed: 300 Km/h Maximum Range: 1,200 Km
Cargo Hold Volume: 12 M³ Wingspan: 17 M
Takeoff & Landing Runway: ≤100 Meters Stall Speed: Extremely Low
Fuel Consumption: 30% Savings Overhaul Interval: 2,000 Flight Hours

Product Description

ES1000 1 Ton-Class Hybrid Ultra-Short Takeoff and Landing Unmanned Transport Aircraft
Core Performance Specifications
  • Maximum Takeoff Weight: 4,500 kg
  • Rated Payload: 1,500 kg (1.5 tons)
  • Cruising Speed: 300 km/h
  • Maximum Range: 1,200 km
  • Cargo Hold Volume: 12 m³
  • Wingspan: 17 m
  • Takeoff & Landing Runway Requirement: ≤100 meters, compatible with gravel, grassland, temporary highways and other unpaved surfaces
  • Airworthiness Design Standard: CCAR-23 Civil Aviation Regulations
Key Performance Features
USTOL Ultra-Short Takeoff & Landing

Equipped with distributed electric propulsion and wing blown lift augmentation technology. Eight sets of electric propellers are arranged on the wings; downwash airflow greatly improves low-speed lift capacity with an extremely low stall speed. The aircraft can operate with only a 100-meter short runway, eliminating reliance on standard civil airports.

Turbine Hybrid Power System

The power system adopts a turbine aero-engine for power generation driven by multiple electric motors, delivering over 30% fuel savings compared with traditional fuel-powered fixed-wing transport aircraft of the same tonnage. Electric propulsion effectively reduces noise during low-altitude flight.

High-Reliability Intelligent Autonomous Flight Control

Full autonomous flight solution supports one-click route planning, automatic takeoff/landing, intelligent obstacle avoidance and remote real-time monitoring. Equipped with the PHM Prognostics and Health Management system for continuous monitoring of operating status.

Lightweight Composite Airframe

The fuselage adopts a hybrid structure of carbon fiber composite materials and aerospace-grade aluminum alloy, featuring lightweight design and ample payload margin. Strong corrosion resistance and fatigue resistance adapt to harsh operating environments.

Core Competitive Advantages
Dual Strength in Payload & Range

With a 1.5-ton rated payload and 1,200-kilometer maximum flight range, this aircraft enables a three-tier air logistics network connecting main airports, county-level regional hubs and township terminals.

Minimal Site Infrastructure Investment

Only needs a 100-meter flat temporary site, with no requirement for constructing dedicated general aviation airports. Operators can leverage rural highways, mine temporary yards and island flat grounds.

Proven Commercial Feasibility

The aircraft has passed comprehensive bench testing and structural static strength verification, with a stable supporting supply chain covering avionics and power systems.

Multi-Scenario Versatility

Beyond regional freight transportation, the platform can be refitted for multiple missions: emergency relief material airdrop, forest fire retardant spraying, high-altitude medical supply delivery, and border patrol.

Operation & Maintenance Cost Analysis
Direct Single-Flight Operating Cost
  • Energy & Fuel Cost: $17.5 to $23.5 per ton per 100 kilometers
  • Labor Cost: Fully unmanned operation only requires 2 ground staff
  • Site Usage Cost: Annual site operating expense under $7,200
Annual Routine Maintenance Expense
  • Condition-Based Intelligent Maintenance: 6% to 8% of aircraft's total purchase price
  • Low-Consumption Power System: Turbine generator overhaul interval of 2,000 flight hours
  • Low Structural Maintenance: Carbon fiber airframes free from rust and corrosion
Investment Payback Cycle

Assuming full 1.5-ton payload, 2 daily round trips with 300 km one-way distance, net profit per single trip ranges from $4,200 to $7,000. Investment payback period ranges from 3.5 to 5 years under standardized commercial operation.

Objective Limitations
  • As a fixed-wing USTOL aircraft, vertical takeoff and landing capability is not available. A 100-meter flat ground is still required.
  • Type certification is currently in progress; full cross-regional commercial route operation will be available upon official airworthiness approval.
  • For short-haul routes within 200 km, the unit freight cost cannot compete with small multi-rotor UAVs.

Product Highlights

ES1000 1.5-ton payload hybrid USTOL unmanned transport aircraft with 1,200 km range. Features ultra-short 100m takeoff/landing on unpaved surfaces, 30% fuel savings, autonomous flight, and CCAR-23 airworthiness design. Ideal for regional logistics, emergency relief, and multi-scenario operations with minimal infrastructure investment.

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