Mitsubishi DA-U210

Brand: Mitsubishi

The Mitsubishi DA-U210 is a reusable rocket engine that is designed for the second stage of the H-2A and H-2B launch vehicles. It uses a combination of liquid oxygen (LOX) and liquid hydrogen (LH2) as its propellants, which results in a specific impulse of approximately 454 seconds, making it one of the most powerful and efficient engines currently in use for space launches. The engine features a thrust vector control system that allows for precise steering and control during liftoff and ascent, as well as an advanced turbopump system that provides reliable and consistent performance.

• Power Output: 25W into 8Ω (stereo)
• Frequency Response: 10Hz to 60kHz
• Distortion: 0.1%
• Damping Factor: 25
• Speaker Impedance:
• Input Sensitivity: 1mV (mic), 2.5mV (mm), 150mV (line)
• Signal to Noise Ratio: 74dB (mm), 100dB (line)
• Line Output: 150mV (line), 50mV (din)
• Dimensions: 425 x 139 x 324 mm
• Weight: 8 kg
• Year:
• Price: