190
this post was submitted on 27 Jul 2023
190 points (97.0% liked)
Technology
58303 readers
18 users here now
This is a most excellent place for technology news and articles.
Our Rules
- Follow the lemmy.world rules.
- Only tech related content.
- Be excellent to each another!
- Mod approved content bots can post up to 10 articles per day.
- Threads asking for personal tech support may be deleted.
- Politics threads may be removed.
- No memes allowed as posts, OK to post as comments.
- Only approved bots from the list below, to ask if your bot can be added please contact us.
- Check for duplicates before posting, duplicates may be removed
Approved Bots
founded 1 year ago
MODERATORS
you are viewing a single comment's thread
view the rest of the comments
view the rest of the comments
I don't see much of a difference between this and current technology. NASA has been using nuclear reactors in probes and rovers for quite some time. Presently deep space probes use nuclear reactors to generate electricity. Propulsion is produced by using electricity to accelerate ions. The ions come from gas stored in cold liquid form.
I don't see any breakthrough technology here. From what I can tell reading the article, it's just a lightly different way of creating propulsion, pressurizing the gas with heat instead of accelerating it with an electromagnetic field. Seems like a step back actually.
Some satellites and rovers have used Radioisotope Thermoelectric Generators (RTGs), which are very different from a nuclear reactor. They use polonium-210, which generates heat, and that heat is converted to electricity with thermocouples. They are low power and inefficient.
To my knowledge no satellite, with an RTG, has ever used ion propulsion. Few interplanetary satellites have ever even used ion thrusters. Dawn, Hayabusa, and Deep Space 1 are the only I can think of, and they all used solar arrays.
Ion thrusters are super efficient, but produce extremely small amounts of thrust. They aren't practical for getting large spacecraft to Mars. These proposed nuclear engines produce large thrust while have efficiency somewhere between regular chemical propulsion and ion propulsion.