On Thu, 1 Aug 2002 [EMAIL PROTECTED] wrote: > << If you're talking about a flyby as the asteroid passes -- so the probe > just needs to be in the right near-Earth place at the right time -- then a > reasonable rule of thumb is to take an orbital delta-V and add 3km/s. > > Ditto for close ones. Maybe add another km/s to catch pop-ops outside the > Moon's orbit...
If you get modest advance warning, you need very little beyond escape velocity, because even a very slight excess at injection altitude translates to quite a bit after escape. (For example, escape plus 50m/s near Earth leaves you heading out at over 1000m/s after escape, which puts you far beyond the Moon in a week.) You need large excesses only if it's very short notice and you really need to cover the distance to the rendezvous point quickly. (An extra 1km/s near Earth translates to nearly 5km/s after escape, which puts you beyond the Moon in less than a day.) Henry Spencer [EMAIL PROTECTED] _______________________________________________ ERPS-list mailing list [EMAIL PROTECTED] http://lists.erps.org/mailman/listinfo/erps-list