[net.space] Light Sail Deployment

peterb@pbear.UUCP (02/25/85)

	Regarding light sails,

	I don't know if mylar is the best, but I  think  that  it
will work quite well.

	When building a  light  sail,  there  are  a  few  design
 problems  that  have  to be overcome, such as weight (obviously)
 rigidity, ease of deployment,  and  resistance  to  damage  from
 micro  meteors.   I  remember  a  story called "Sun Jammer" that
 described an earth to moon race by solar yachts.   These  varied
 in  design,  and  the  story  described  quite  a  bit about the
 problems of solar sails.

	One of the problems is how do you deploy a sail that is a
few miles in surface area, and then once deployed how do you keep
it in shape.

	One of the obvious ideas it to  spin  the  sail  and  use
centrifical  force  to  keep  the sail in place while it is being
deployed.  This is assuming that the sail has been  packed  in  a
tube  with  the shrouds to be released first and then as the tube
rotates the rest of the sail pulls it self out.  Also  the  speed
of  rotation  would  drop as more and more sail is released until
the entire sail is released.

	Once released and spinning the sail would form  a  circle
with  a  depressed  center  (from  photon pressure) and has to be
strutted in order for it to keep its shape for  a  few  millenia.
One  idea  I  thik  would  work is to us an foaming agent that is
released into mylar tubes that are bonded to the  sail  (backside
so as not to interfere with the mirror).  As the foam expands, it
would  rush  to  the  extreme  end of the tube that is exposed to
vacuum.  Also the centrifical force would help  it  on  its  way.
Then  the foam would vacuum cure and become rigid.  This may be a
little messy, but it would be quite simple in design.   Also  the
tubes would not have to worry about crimping since the foam would
expand  slightly  as  it  cured and cause the tubes to assume the
largest volume (a circle).

	The tubes can all be connected to a central valve at  the
apex  of  the  sail  and  once the foam is injected and cured the
deploment tube can jus cut itself away and the sail  would  start
on its journey.

	Steering the sail would be difficult, and  I  don't  have
the  answers to that one.  I would wish someone would pick up the
idea and bounce it around.

					Peter Barada
					ima!pbear!peterb

karn@petrus.UUCP (02/27/85)

Does anyone know just how high you have to be to construct a "high
performance" solar sail? Aside from atmospheric drag (which makes
your average space shuttle orbit useless) there is also a rather
large gravity gradient at low altitudes which might rip a delicate
sail.

Phil

al@ames.UUCP (Al Globus) (02/28/85)

> 	Steering the sail would be difficult, and  I  don't  have
> the  answers to that one.  I would wish someone would pick up the
> idea and bounce it around.
> 
> 					Peter Barada
> 					ima!pbear!peterb

With all this talk about solar sails on the net I thought you might like
to know that the World Space Foundation is actually building one and
expects to fly it.  The have built two prototypes, one full size, and have had
an upper stage donated to them.  They still need a launch - either shuttle
or Ariane - and I don't think they've started on the flight article.
They main players are experienced people from JPL, they know what 
they're doing.  

I don't know how far they've got on control, but the 
last I saw there were two small rotatable sails on the end on one of
the booms for pitch and roll control.  There is also a movable mass near
the center of the sail for yaw.

If anyone has the address available, why don't you post it?  Most of
their labor is volunteer.  If you want to help, contact Robert Staehle (sp?)
at JPL in Pasadena, CA.

karn@petrus.UUCP (03/04/85)

> With all this talk about solar sails on the net I thought you might like
> to know that the World Space Foundation is actually building one and
> expects to fly it.  The have built two prototypes, one full size, and have had
> an upper stage donated to them.  They still need a launch - either shuttle
> or Ariane - and I don't think they've started on the flight article.
> They main players are experienced people from JPL, they know what 
> they're doing.  
> 
> I don't know how far they've got on control, but the 
> last I saw there were two small rotatable sails on the end on one of
> the booms for pitch and roll control.  There is also a movable mass near
> the center of the sail for yaw.
> 
> If anyone has the address available, why don't you post it?  Most of
> their labor is volunteer.  If you want to help, contact Robert Staehle (sp?)
> at JPL in Pasadena, CA.

The World Space Foundation is indeed a serious group. They have approached
AMSAT, the radio hams who build amateur communications satellites and
have proposed a joint venture in which AMSAT builds the communications
hardware to fly on their sail. They get command, telemetry and tracking
facilities, something that AMSAT can do well, and we (AMSAT) get a slow
but free ride for a transponder into a useful communications orbit, something
that AMSAT is always looking for.

We were all impressed with their technical knowledge of the subject, and
they seem to have a viable organization. A possible joint project
is only in the very preliminary stages at the moment, but one thing that
can make it emerge into reality very fast is for volunteers to step forward
and actually take on part of the design job.  The primary contact person on
the AMSAT side for the project is Dr. John Champa, K8OCL. John recently moved
to Michigan and I don't have his new address handy, but mail to him can be
forwarded via the AMSAT address (PO Box 27, Washington, DC 20044).  Feel free
to contact him if you think your interests might lie in the electronics
side of such a project. Here's YOUR opportunity to do something "up there"
besides talk about it idly on net.space!

Regarding photon pressure and spinning toys: AMSAT-Oscar-7, launched in
1974, made practical use of this phenomenon. In those days, amateur
satellites had no propulsion systems or active attitude control systems,
but something had to be done to keep them from tumbling uncontrollably.
The end-over-end motion was easy enough, you just stick a big bar magnet
along the main axis of the spacecraft. Within days after launch the
whole thing aligns itself with the earth's magnetic field and the satellite
turns end-over-end slowly twice per orbit (this is a polar orbit).
The remaining problem was to control roll about the magnet axis, and for
this task photon pressure was used. The satellite had four antenna elements
bent towards one end, which were fabricated out of ordinary carpenter's
rule (the kind that's yellow or white, with inch markings). One side of
each element was painted white, the other black.  The result was a net
torque from radiation pressure that slowly rolled the spacecraft about
its magnet axis at almost exactly the predicted rate. Very simple, very
effective.

Phil Karn
Asst. VP Engineering, AMSAT