1. Scope of aplication: Rocket nozzle air tightness test
2. Technical parameters:
Maximum hydraulic pressure range: 60MPa (Pressure level optional 60/120/160/300)
Maximum pneumatic pressure range: 35MPa
Constant pressure control accuracy: ±1%
Test interface: 1 channel (connecting test piece, internal four channels, three channels liquid, one channel gas)
Medium: Distilled water or hydraulic oil/compressed air or nitrogen