This transcription has been completed. Contact us with corrections.
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)