Objective

The GIESEPP (Gridded Ion Engine Standardised Electric Propulsion Platform) project will develop, build and test to TRL5 the first European Plug and Play Gridded Ion Engine System to operate ArianeGroup and QinetiQ Space Ion Engines for LEO, GEO and Space Exploration Missions.

What does Gridded Ion Engine Technologies stand for?

Gridded ion thrusters are part of the electrostatic electric propulsion thrusters. The ion thruster generate thrust in two steps. In the first step ion thrusters employ a variety of plasma generation techniques to ionize a large fraction of the propellant. In the second step the ionized fraction of the propellant is accelerated in an electrostatic field of the grid system. The ion acceleration in a grid system is the common feature of all gridded ion engines. An ion thruster consists of basically three components: the plasma generator, the accelerator grids, and the neutralizer cathode.

Organisation

GIESEPP project needs and team Involvement.
The project is structured based on the following team member responsabilities:

  • Satellite System Requirements:
    OHB
  • Thrusters:
    ArianeGroup/ QinetiQ
  • System Engineering:
    ArianeGroup/ QinetiQ
  • PPU:
    Airbus Defence and Space / Crisa
  • Propellant Control:
    AST
  • Testing:
    QinetiQ / ArianeGroup
  • Analytical Design and Test Support:
    Mars Space
  • Alternative Propellants:
    University of Southampton

Schedule

Project Schedule

The project has an overall duration of 48 months and is subdivided in 5 Phases.

Phase 1 (months 1–7)
Mission Scenarios, Platforms, Requirements and Gap Identification

Phase 2 (months 7–16)
Electric Propulsion System Definition

Phase 3 (months 16–24)
Electric Propulsion System Development and Cost Optimization

Phase 4 (months 24–36)
Build, Procure, Assemble and Prepare Standardised Tests

Phase 5 (months 36–48)
Test and Analysis

Phase 1
Phase 2
Phase 3
Phase 4
Phase 5