Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!mnetor!seismo!ll-xn!mit-eddie!husc6!husc2!chiaraviglio From: chiaraviglio@husc2.UUCP (lucius) Newsgroups: sci.space Subject: Re: why Mercury (liquid metal) used for ion rocket? Message-ID: <1005@husc2.UUCP> Date: Sun, 2-Nov-86 00:30:02 EST Article-I.D.: husc2.1005 Posted: Sun Nov 2 00:30:02 1986 Date-Received: Mon, 3-Nov-86 22:42:43 EST References: <8610310012.AA13920@s1-b.arpa> Organization: Harvard Univ. Science Ctr., Cambridge, MA Lines: 15 Summary: Specific impulse depends on molecular weight only in adiabatic expansion-driven propulsion systems. My understanding of the way that ion drives work is that they accelerate the ions out backwards electrostatically, a procedure that is not temperature-dependant, and thus will lose no more energy in unuseable heat for large-molecular-weight substances than small-molecular-weight substances. Therefore, other factors are the considerations in choosing a propellant. -- -- Lucius Chiaraviglio lucius@tardis.harvard.edu {insert your favorite brave system here}!seismo!tardis!lucius Please do not mail replies to me on husc2 (disk quota problems, and broken mail system won't let me send mail out). Please send only to the address given above.