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- Newsgroups: sci.space
- Path: sparky!uunet!zaphod.mps.ohio-state.edu!cs.utexas.edu!torn!utzoo!henry
- From: henry@zoo.toronto.edu (Henry Spencer)
- Subject: Re: A solution to "NASA Coverup"? (long)
- Message-ID: <BxDsps.AF7@zoo.toronto.edu>
- Date: Sun, 8 Nov 1992 05:03:27 GMT
- References: <BxDoxB.5u0.1@cs.cmu.edu>
- Organization: U of Toronto Zoology
- Lines: 24
-
- In article <BxDoxB.5u0.1@cs.cmu.edu> roberts@cmr.ncsl.nist.gov (John Roberts) writes:
- >... After firing to escape low earth orbit, the spacecraft is moving
- >in nearly a parabolic or hyperbolic (probably parabolic, but I'm not sure -
- >it depends on velocity) trajectory, which gradually changes to a (probably)
- >hyperbolic trajectory about the moon...
-
- A lunar trajectory actually starts out as an ellipse with a very high
- apogee; reaching parabolic velocity is not (quite) necessary. It does
- look like a hyperbola around the Moon once you get close enough, although
- you really have to be pretty close for the Earth's effects to be negligible.
-
- >...Remember that the moon is orbiting about the Earth at a
- >velocity of around 1023 meters per second (avg) - if it takes the spacecraft
- >several days to get from Earth orbit to the moon, the moon will have traveled
- >a tremendous distance "sideways" during that time...
-
- Whence my comment about it being better to ignore the Moon entirely than to
- assume it is motionless. There *is* an exact solution for the three-body
- problem if you assume two primary bodies motionless with respect to each
- other and a negligibly small third body -- it's called Euler's Problem Of
- Fixed Centers -- but it's pretty useless in practice.
- --
- MS-DOS is the OS/360 of the 1980s. | Henry Spencer @ U of Toronto Zoology
- -Hal W. Hardenbergh (1985)| henry@zoo.toronto.edu utzoo!henry
-