fisher@dvinci.DEC (Burns Fisher, MRO3-1/E13, 231-4108) (04/20/84)
NO! There is absolutely no fuel left on board for the SSMEs (Space Shuttle
Main Engines) after the ET (External Tank) drops. The SSMEs are not started
again until the next launch. As a sanity check on this assertion, think of
what you would have to do to save any reasonable quantity of liquid H2 and
liquid O2. (Insulation, high pressure tanks, etc etc). Also think of how
little energy is actually required to start the reentry process as compared
to the amount required to get up into orbit to begin with. Using the SSMEs
for deorbit does not make sense!
Here are the major engines on the shuttle and their acronyms (in order of
power):
SRBs (Solid Rocket Boosters) - millions of pounds thrust. Used only
during first (1.5?) minutes after launch, then dropped off and
recovered.
SSME (Space Shuttle Main Engines) - 10**5s of pounds thrust. Used
from launch until just before orbital insertion. Draws fuel
from ET (external tank) which is dropped just after the SSMEs
stop. Not used again until the next launch.
OMS (Orbital Maneuvering System) - 10**3s of pounds (?) thrust. Used
to insert the shuttle into a reasonable orbit after the SSMEs
stop. (OMS-1 and OMS-2 [OMS-1 was omitted during the last
mission, because of the unusual trajectory/burn time planned
for the SSMEs-required for the unusually high orbit]) Also
used for orbital changes during the mission (e.g. rendezvous
etc.), AND FOR DEORBIT BURN (retrofire for us old-timers).
RCS (Reaction Control System) (isn't every rocket?). - Small thrust.
Used to change or maintain orbiter attitude while on orbit.
Also can be used to make small orbital corrections for
station-keeping or final phases of rendezvous. Also used
during the early phases of reentry for attitude control in
various combinations with the control surfaces depending on
the thickness of the atmosphere.
RMS (Remote manipulator system). The "robot arm". Not an engine.
Burns (picky picky) Fisher
<Is this coming close to being a flame? Sorry...>
UUCP: ... {decvax|allegra|ucbvax}!decwrl!rhea!dvinci!fisher
ARPA: decwrl!rhea!dvinci!fisher@{Berkeley | SU-Shasta}mat@hou5d.UUCP (04/21/84)
I believe that the SRB's each generate about 2.7 million lbs (what's that in
Newtons?) of thrust. The three ``main engines'' contribute about another 1.4
million lbs. Total: A little over 7 million lbs. This is assuming the second
generation SRBs and the 104% thrust liquid engines.
Compare this with the Saturn V used on the last moon shot. Total thrust from
five engines: about 7,780,000 lbs. The center engine was either a little more
or less powerful than the others in order to avoid both excess stress to the
structure of the booster and a troublesome reverse-direction gas flow under
the booster. The main booster and second stage put 300,000 lbs in earth orbit!
We've got to take the shuttle a bit further before it will be really ready
to pave the way into space.
--
from Mole End
Mark Terribile
(scrape..dig) hou5d!mat
,.. .,, ,,, ..,***_*.