[net.space] Electric rockets

David.Smith@CMU-CS-IUS@sri-unix.UUCP (08/05/83)

There is another type of electric rocket (besides ion) which has
been used for attitude stabilization.  It involves a block of teflon
and an electrical spark.  The spark vaporizes a bit of teflon, which
then goes flying out the nozzle.  AW&ST carried an article on it --
what, several moons ago?  In actual use on a spacecraft, the things
were fired several times a second over some years.  Very low thrust,
but not much is needed for this application.

Incidentally, the latest AW&ST (that I have seen) has a picture
of the meteroid hit on Challenger's windshield which forced the
glass to be replaced.

karn@eagle.UUCP (Phil Karn) (08/07/83)

Speaking of electric rockets, AMSAT has come up with a similar rocket that
could be used on a future payload launched from a GAS can on the
shuttle.  The problem here is that you want an engine to boost the
payload into a longer lived orbit than 300 km, but to prove to the NASA
people at the same time that it is intrinsically safe to fly on a manned
vehicle.

The proposal is to fly a steam rocket.  Liquid water is directly preheated
with solar energy and fed to a thrust chamber where an electrically
powered heater turns it to steam.  Specific impulse is terrible (~140 sec)
but mass isn't a limitation; only a couple tens of kilograms of water
would be required for the job.

Of course it would be much easier and quicker to just carry two solid
rocket motors to perform a two-impulse Hohmann transfer to the higher
circular orbit, but just getting permission from NASA to deploy
something from the GAS can will be a major accomplishment.

Phil