Paratus
Lifer
- Jun 4, 2004
- 17,754
- 16,093
- 146
The TLDR from the link above.
They tested the thruster at:
The tests showed two signals. One that appeared to be thermal and another that appeared to be thrust.
They found thrust in the forward direction of ~1.2mN/kw
They found thrust in the reverse direction of ~1.2mN/kw
(Hall effect plasma thrusters are ~60mn/kw, laser and solar sails are two orders of magnitude lower than this thruster)
In the null direction they only saw the thermal effects. The signal was significantly different than either the forward or reverse.
They calculated the uncertainty due to thermal, electric, mechanical, sensor error, @
& magnetic effects to be about +6uN absolute. (Absolute thrust measurements were 40-119uN for comparison)
Test was done for proof of concept not to optimize thrust/kw.
They tested the thruster at:
- 40, 60, & 80W in the forward direction
- 40, 60, & 80W in the reverse direction
- 80W in the null direction
The tests showed two signals. One that appeared to be thermal and another that appeared to be thrust.
They found thrust in the forward direction of ~1.2mN/kw
They found thrust in the reverse direction of ~1.2mN/kw
(Hall effect plasma thrusters are ~60mn/kw, laser and solar sails are two orders of magnitude lower than this thruster)
In the null direction they only saw the thermal effects. The signal was significantly different than either the forward or reverse.
They calculated the uncertainty due to thermal, electric, mechanical, sensor error, @
& magnetic effects to be about +6uN absolute. (Absolute thrust measurements were 40-119uN for comparison)
Test was done for proof of concept not to optimize thrust/kw.

