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Engines

RT1200

The RT1200 quad-rotor rotary engine offers exceptional power density in a compact 1.2 L displacement package. Designed for high performance, it delivers rich torque, liquid cooling and streamlined integration for advanced aerospace and UAS platforms.

Rotron RT1200 Quad Rotor Wankel EngineRotron RT1200 Quad Rotor Wankel Engine
Key Features

Unlocking new potential in rotary engine design

Max Peak Power
200HP
Max Peak RPM
7500RPM
Max Continuous
150HP
Engine Weight
54KG
(119 LBS)
Engine Type
Quad Rotor
Rotary Engine
Displacement
1200cc
Fuel Type
Unleaded 95 Octane
Avgas 100LL
Fuel Consumption
0.56LBS
/ Per HP / Per Hour
OVERVIEW

With up to 200 hp peak output and 150 hp continuous capability, the RT1200-P supports demanding missions. Its lightweight design and modular integration flexibility make it suited for heavy-duty VTOL, UAS and prototype propulsion solutions.

Explore the interactive hotspots below to learn more about the 
RT1200
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Rotron RT1200 Rotary Engine
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Technology

The RT1200’s quad-rotor Wankel architecture minimises reciprocating mass and vibration while producing an expansive power curve. Combined with liquid cooling, electronic fuel injection and refined rotor dynamics, it delivers class-leading power-to-weight, smooth performance and extended operational durability for endurance and high-payload use-cases.

Rotron RT1200 Quad Rotor Wankel Engine
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Maximum Output Design: Quad-rotor rotary configuration enables peak 200 hp power delivery and formidable torque across the rpm band.

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Optimised Thermal & Mechanical Efficiency: Liquid-cooling and minimal vibration architecture reduce component stress, enhance endurance and support sustained high-load operation.

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Optimised Form-Factor: Compact layout and flexible mount/drivetrain compatibility allow installation in tight envelope UAS, VTOL, or manned light-aircraft systems.

Range

Fan-drive system range.

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in use & partnership with
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Features

High-Power Quad-Rotor Propulsion Engine for Heavy-Duty UAV and VTOL Platforms

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Quad‑rotor power architecture
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Exceptional power density
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Advanced engine design
Quad‑rotor power architecture

The RT1200‑P uses an advanced quad-rotor rotary configuration to deliver exceptional power density and smooth performance in a compact package. Its four rotors provide a broad power curve and strong torque up to 200 hp, supporting demanding flight profiles with responsive, controlled output. This innovative design preserves the smoothness and reliability of rotary engines while offering a high-performance solution that integrates seamlessly into advanced platforms.

Rotron RT1200-P Quad-Rotor Architecture
Exceptional power density

With a 1,200 cc displacement and 200 hp from just 54 kg, the RT1200‑P sets a new benchmark for power-to-weight ratio. Its compact design frees space and mass in the airframe, allowing optimised payload, fuel load or aerodynamics. This high-density performance delivers greater mission flexibility and efficiency, making it ideal for advanced unmanned and experimental aviation platforms.

Rotron Rt1200-P - High power-to-weight performance
Advanced engine design

The RT1200‑P’s advanced rotary design combines liquid cooling, precision fuel injection and refined Wankel dynamics to deliver peak power with minimal vibration and wear. Its thermally stable, smooth operation supports a 1,000‑hour TBO, providing long-term durability in high-usage environments. This endurance-focused engineering ensures reliable, efficient performance for platforms where operational economy and dependable service life are critical.

Additional Details

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Specifications

Full specifications

Rotron RT1200-P Engine Dimensions
Technical Specifications
Engine Type
Quad [4] Rotor, Rotary
Displacement
1200cc
Application
Prototype
Max. Peak
200HP
Max. Peak RPM
7500RPM
Max. Continuous
150HP
TBO
1000Hrs
System Weight
54 KG / 119 LBS
Drive Type
Direct Drive
Drive Rotation
Counter-Clockwise
Fuel System
Fuel Injection
Fuel Type
Unleaded 95 Octane / Avgas 100LL
Fuel Consumption
0.56 LBS / Per HP / Per Hour
Cooling
Liquid Cooling
Starting Device
Electric Onboard
Ignition System
Programmable fuel injection with CAN bus
Generator
700W 12V
Rotron RT1200-P Engine Dimensions
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DATA

Performance Data

Max Peak Power
200HP
@ 7500 RPM
Max Continuous Power
150HP
(continuous rating)
Fuel Consumption
0.56 LBS
/ Per HP / Per Hour
Performance Data
Rotron RT1200 Engine Performance Data
FAQ

Frequently
Asked Questions

What is the displacement and configuration of the RT1200-P?

The Rotron RT1200-P is a quad-rotor engine with 1,200 cc combined displacement.

What rated power output does the RT1200-P deliver?

The RT700-XE delivers up to 200 hp peak, with continuous capability around 150 hp.

What drives and rotation direction are supported?

Direct-drive configuration; rotation is counter-clockwise (viewed forward).

What fuel system and fuel types are used?

The R1200-P operates an electronic fuel injection is standard; compatible with 95 octane unleaded or Avgas 100LL.

What is the fuel consumption figure?

The RT700-XE operates at approximately 0.56 lbs per hp-hour under typical cruise conditions.

What cooling and starting systems are included?

A liquid-cooling loop is used; engine includes onboard electric starter.

What is the quoted TBO (Time Between Overhauls)?

The engine architecture supports up to 1,000 hours, depending on mission profile and duty cycle.

How does the RT1200-P suit heavy-duty and high-endurance environments?

Its large displacement, quad-rotor layout, low vibration and compact footprint enable integration into high-payload UAVs, VTOL craft and prototype aerospace systems.

Can the RT1200-P interface with external electrical or telemetry systems?

Yes. The RT1200-P supports drivetrain and generator integrations to deliver onboard power and telemetry data compatibility.

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