Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
LGIT

LGIT

LGIT

UM electric rocket engine. Linear Gridless Ion Thruster, a two-stage device designed to incorporate the efficient ionization process of gridded ion thrusters and the high thrust density of Hall thrusters.

Thrust: 0.0200 N (0.0040 lbf). Specific impulse: 1,400 s.

The Linear Gridless Ion Thruster (LGIT) was a two-stage device that was designed to incorporate the efficient ionization process found in gridded ion thrusters with the high thrust density and crossed-field acceleration mechanism of Hall thrusters. This thruster essentially combined the ionization stage of an ion thruster with the acceleration stage of a Hall thruster. Initial tests of the LGIT were disappointing. In the three minutes that the discharge was maintained, the thrust stand recorded a constant thrust of approximately 20 mN. This equated to a specific impulse of approximately 1400 seconds. The calculated anode efficiency was 12%. The low efficiency was not surprising considering that the LGIT was operating in a single-stage mode rather than the two-stage mode for which it was designed.

Electrical Input Power: 2.00 kW.



Country: USA. Agency: UM.

Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use