Re: Striking a Lunar target in the near future...

From: John Schilling (schillin_at_spock.usc.edu)
Date: 08/21/04


Date: 21 Aug 2004 10:54:06 -0700

Bryan Derksen <bryan.derksen@shaw-spamguard.ca> writes:

>On 19 Aug 2004 15:31:59 -0700, thomsona@flash.net (Allen Thomson)
>wrote:
>>The far side Tsiolovski Evil Object is a somewhat different
>>target, and obviously harder. Probably you'd want to have a
>>couple of satellites/probes in sight of it and the earth to
>>help the nuke get where it's going.

>Another proposal elsewhere in this thread involved gutting a
>geosynchronous communications satellite that was already in the
>pipeline for launch to serve as a lunar transfer vehicle. Would any
>existing comm sats already in geosynchronous orbit have enough onboard
>fuel to get them out into the vicinity of the Moon to act as a
>communication relay for a farside strike?

Unfortunately no. A communications satellite sitting on the launch
vehicle, has enough propellant to reach Lunar orbit. Even in the
transfer orbit that takes it to geostationary orbit, you can wait
a few weeks for everything to line up and turn what should have been
the GEO circularization burn into an insertion burn for a translunar
orbit. This is what Boeing did with HGS-1 a few years back, to get
the lunar gravity assist when a third-stage malfunction meant that
they couldn't reach GEO directly.

But once you're actually in GEO, you've burned that fuel and all you've
got left is a modest allowance for stationkeeping. Even for a brand
new late-model comsat, that's at least a factor of three low for a
lunar mission.

-- 
*John Schilling                    * "Anything worth doing,         *
*Member:AIAA,NRA,ACLU,SAS,LP       *  is worth doing for money"     *
*Chief Scientist & General Partner *    -13th Rule of Acquisition   *
*White Elephant Research, LLC      * "There is no substitute        *
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*661-718-0955 or 661-275-6795      *    -58th Rule of Acquisition   *


Relevant Pages

  • Bizarre Lunar Orbits
    ... Bizarre Lunar Orbits ... PFS-2 to orbit the Moon about every 2 hours. ... The orbit of PFS-2 rapidly changed shape and distance from the Moon. ...
    (sci.space.news)
  • Re: Next X
    ... lunar transfer speed. ... Indonesia respectively - for a more normal equatorial orbit. ... 910 sec Isp - laser thermal stage ... A 3000 metric ton vehicle -launches 490 tons into LEO. ...
    (sci.space.policy)
  • Re: Improved lunar landing architecture
    ... >lunar orbit. ... >two launches put up a lunar orbiting CEV, ... NASA instead prefers to build up slowly. ... With my approach the crew would of course only leave the ...
    (sci.space.policy)
  • Re: Next X
    ... lunar transfer speed. ... Indonesia respectively - for a more normal equatorial orbit. ... 910 sec Isp - laser thermal stage ... A 3000 metric ton vehicle -launches 490 tons into LEO. ...
    (sci.space.policy)
  • Re: lunar centric orbit?
    ... >but what are the parameters of lunar centric orbit? ... we don't seem to know squat about the aspects of any "lunar ... Although being a fully interactive zone in a good sort of way, ...
    (sci.space.policy)