Pros:
o The missiles take 1/2 hour to fuel, so their military usefulness
is limited at best (first strike, anyone?)
o They don't have to be moved; just remove the warhead bus and
replace with a satellite & shroud & ... (I didn't say this
was free or even cheap; just available soon)
Cons:
o Are they reliable enough to use as satellite launchers?
o Would the Soviets be nervious if they saw a (single)
launch of a Titan II into circum-polar orbit? [i.e.,
would they think it's a pin-down strike?]
o Military: We can't spare a single missile.
Unknowns:
o Cargo weight of a Titan II to LEO? to GSO?
o Time to build a housing for a satellite for the Titan II?
Anyway, if anyone knows more about this than I (That is to say,
any real facts), I would be curious about this.
--
-- Bob Gottlieb
UUCP: ...!linus!alliant!gottlieb
Mail: Alliant Computer Systems Corp, 42 Nagog Park, Acton, MA 01720
Phone: (617) 263-9110
Foot: "You can't get there from here".
---------------------------------------------------------------------------
"I don't know what I'm doing, and Alliant isn't responsible either, so there!"
As I recall, the USAF is way ahead of you, and already plans to use some
of them for satellite launches.
> o The missiles take 1/2 hour to fuel, so their military usefulness
> is limited at best (first strike, anyone?)
Can you cite a reference for this? The Titan II, unlike the long-gone
Titan I, uses room-temperature propellants specifically so that it can sit
in the silo fully fuelled.
> o They don't have to be moved; just remove the warhead bus and
> replace with a satellite & shroud & ...
No, they do have to be moved. Missile silos are sited without much concern
for range safety; if those things are going up, nobody is going to be too
worried about where the spent stages will land, or where the rocket might
go if something fails. That isn't acceptable for peacetime space launches.
> o Are they reliable enough to use as satellite launchers?
Should be. The Titan launchers are only modest variants of the ICBMs.
One early variant was used for the Gemini manned missions.
> o Would the Soviets be nervious if they saw a (single)
> launch of a Titan II into circum-polar orbit? [i.e.,
> would they think it's a pin-down strike?]
This is another reason why it's smart to launch from an existing launch site
on well-known launch paths, rather than straight from silos. Early-warning
radars aren't necessarily capable of counting the missiles or precisely
identifying where they are headed.
> o Cargo weight of a Titan II to LEO? to GSO?
Into LEO, comparable to a Gemini spacecraft, since it's the same rocket.
Clarke orbit, maybe not a lot.
> o Time to build a housing for a satellite for the Titan II?
Probably not too hard, since there are payload shrouds already in use for
the assorted Titan space-booster variants. Martin Marietta's commercial
Titan will probably use essentially stock Ariane shrouds.
--
Henry Spencer @ U of Toronto Zoology
{allegra,ihnp4,decvax,pyramid}!utzoo!henry
Please digress further! I, for one, would be very interested in a comparison
of American and Soviet missiles. Are liquid fueled or solid fueled boosters
more easily "targeted" during boost phase? As I understand it liquid fueled
has more lift capability. Does that imply a hotter plume? Please, digress!
Jeff McQuinn just VAXing around