EJ-400
A compact reverse-flow turbojet engine with 400 N thrust capability, 98,000 RPM maximum shaft speed and high power density for aerospace platforms.
- 400 N Thrust
- 98,000 RPM
- 100 kW Power
Explore aerospace propulsion systems, ignition technologies, propulsion testing equipment and power engineering solutions developed for demanding technical applications.
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A compact reverse-flow turbojet engine with 400 N thrust capability, 98,000 RPM maximum shaft speed and high power density for aerospace platforms.
An advanced ramjet propulsion concept developed for high-speed aerospace applications and future-oriented propulsion studies.
A high-energy ignition solution designed for ramjet, scramjet, turbojet and high-capacity burner systems under demanding operating conditions.
A precision spark ignition unit developed for controlled aerospace startup cycles and reliable ignition support.
A solid fuel igniter developed for reliable first ignition in turbojet engines and mission-critical aerospace applications.
A TDG system designed to create controlled temperature distribution patterns for propulsion system and engine testing environments.
A test system developed to reproduce near flight-service temperature and flow conditions for ramjet and scramjet engine test setups.
A hydrogen-capable combustion system offering high reliability, stable operation and precise process control for demanding applications.
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