Re: Bielliptic Transfer Orbits
From: Erik Max Francis (max_at_alcyone.com)
Date: 08/26/04
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Date: Wed, 25 Aug 2004 19:25:29 -0700 To: sci-space-tech@moderators.isc.org
Bill Woods wrote:
> You're in an orbit with radius R_1. Boost yourself up to escape
> speed and coast out to infinity. Perform an infinitesimal orbital
> correction to put yourself on the second transfer orbit, which has
> periapsis at your target orbit at radius R_2. When you get there,
> a third boost completes the maneuver.
This idealized orbit is called a biparabolic transfer, by the way.
>>> plot(earth, uranus, BiparabolicTransfer)
Source: Earth
Destination: Uranus
Opportunities:
Opportunity: Earth/Uranus
Angle: 1.94298093744 rad (111.32460739 deg)
Period: 31943224.077 s
Transfers:
Transfer: biparabolic from `Earth' to `Uranus'
Duration: inf s
Burns: 12335.3007772, 2815.06576668 m/s
Course: from `Earth' to `Uranus'
Duration: inf s
Deltavee: 15150.3665438 m/s
-- __ Erik Max Francis && max@alcyone.com && http://www.alcyone.com/max/ / \ San Jose, CA, USA && 37 20 N 121 53 W && AIM erikmaxfrancis \__/ War is a continuation of policy by other means. -- Karl von Clausewitz
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