Equipment is intended for hot tests of high-performance inboard plasmajet engines designed by LPSC (India).

Plasmajet engines testing equipment

Plasmajet engines testing equipment

Plasmajet engines testing equipment

Plasmajet engines testing equipment

To test ion engines, it is necessary to create conditions close to space on Earth. To do this, vacuum chambers of a sufficiently large volume are manufactured with a powerful pumping system, dispersion devices and protection against plasma flow.

For ease of maintenance and operation, the test engine is placed in a pre-chamber, which can be cut off from the main vacuum chamber.

Configuration:

  • General vacuum chamber;
  • Pre-chamber for engine;
  • Carbon lining;
  • Cooling system;
  • Plasma beam trap;
  • Oil free vacuum system;
  • Measurement system;
  • Control system.

Ultimate vacuum

1·10-6 mbar

Dynamic vacuum

2·10-5 mbar

Xenon rate (before modernization)

20 mg/s

Plasmajet engine power (before modernization)

20 kW

Xenon rate (after modernization)

60 mg/s

Plasmajet engine power (after modernization)

60 … 80 kW

Dimensions:

Inside diameter of general vacuum chamber

Length of general vacuum chamber

Inside diameter of pre-chamber

Lengthofpre-chamber

 

6000 mm

9000 mm

2000 mm

2500 mm

Documents

QMS Certificates and permissions Equipment Patents Product overview Support information
Certificate of conformity.sheet 1
Certificate of conformity.sheet 2
Quality certificate. Road equipment
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