Relay-Version: version B 2.10 5/3/83; site utzoo.UUCP Path: utzoo!watmath!clyde!burl!ulysses!harpo!seismo!hao!hplabs!sri-unix!David.Smith@cmu-cs-ius.arpa From: David.Smith@cmu-cs-ius.arpa Newsgroups: net.space Subject: Orbital plane change Message-ID: <516@sri-arpa.UUCP> Date: Mon, 2-Apr-84 13:41:55 EST Article-I.D.: sri-arpa.516 Posted: Mon Apr 2 13:41:55 1984 Date-Received: Mon, 9-Apr-84 05:33:56 EST Lines: 26 My skepticism about using the space station for satellite repair was admittedly from a chemical rocket mindset. How old-fashioned of me not to think of ion rockets. (Previous discussions concluded that a solar sail is not useful below about 1000 miles.) Any low-thrust solution will take quite a while, since to be effective it has to be applied at or near the orbit crossovers. How about the following, for low orbit plane changes. This is based on an article I read in (I think) Astronautics and Aeronautics not too many months ago. Move the perigee to the crossing node, and brake off enough speed to drop it into the sensible (but still very thin) atmosphere. Use wing lift normal to the flight path to effect the plane change. This may take several passes. Once the plane is sufficiently changed, fire at apogee to raise the perigee. Of course, the drag at perigee will drop the apogee, unless thrusters fire during the maneuver. As I recall, they expected lift/drag to be about 4. So you get a major plane change for 1/4 the propellant that would have been required for a purely propulsive maneuver. A boon whether you use chemical or electric propulsion. David Smith P.S. Up with the winged space tug!