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Delta_V
lemmy.world
Delta_V@lemmy.world Joined: 2024-01-02 |
![]() Link: https://news.mit.edu/2026/new-propulsion-system-could-make-tiny-satellites-fast-fuel-efficient-0601
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Delta_V
lemmy.world
Delta_V@lemmy.world Joined: 2024-01-02 |
The paper linked to in the article says the thrusters have a specific impulse of 600s, and a thrust-to-power ratio of about 50 mN/kW. Compared to the xenon ion thrusters used on the Dawn spacecraft, these new multi-mode thrusters produce more thrust, but are significantly less efficient. Dawn's thrusters have a specific impulse of 3,100s and a thrust-to-power ratio of about 36 mN/kW. Even so, it means satellites can be built with one small fuel tank that can power high efficiency electrospray thrusters to make slow maneuvers, or use the same fuel as a monopropellant to quickly get out of (or into) the way of something. ASCENT monopropellant thrusters can have a specific impulse slightly better (240 Isp) than traditional hydrazine monopropellant thrusters (235 Isp). |
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