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6) Thermal tests - 357-01 … SPAR estimates 4-6 hours
for these tests. (Arm should be deployed, slightly
above the bay). Check into PRCS FTO's or
requirements during that period of on-orbit time.
(Power is on to the arm)
7) auto mode sections will be rewritten to eliminate
implication that RCS are to be fired during auto
maneuvers
8) software stops. (all joints go into safing when
one hits a soft stop). SPAR tentatively agrees
we need to look at only one (elbow) they'll
get back to us. This should be done with
GF #5.
9) Orbiter PLT & RMS PLT are both required during IECM
testing
10) direct drive berthing/deployment is in.
11) PFTA capture/release: supported strongly by
SPAR/NRCC. Milt will talk to Bob Becker (MPAD)
to initiate safety study (stability of PFTA
in orbit)