All,
The 2 Perigee contacts were nominal for CMD and TLM. The Inertial maneuver was successful. For these contacts we used 2 strings. The contact on 26 Dec was on String-3 (Primary). We accomplished the following: ATS upload “IBEX_2019_005_o0433a_v1,
SSR Dump, Reset Master Timer and set the downlink from 160k to 320k. The second contact on Dec 27 was on String-2 (Back-up). We did the following: Set SC Clock and reset FDC totals. We have completed the patching and testing of String-1 on 22 Dec 2018. The
plan moving forward is starting Jan 1, 2019 will be on String-1 as primary and string-3 as back-up and string-2 will be ready for patching.
Q1 0.83428400 ActNor.EstInrToBdy[0]
Q2 0.01628180 ActNor.EstInrToBdy[1]
Q3 0.05065630 ActNor.EstInrToBdy[2]
Q4 0.54876100 ActNor.EstInrToBdy[3]
GPS sec
1229947341.000 ActNor.EstTime
MPS Cmd Vector X 0.108493000
MPS Cmd Vector Y -0.907965000
MPS Cmd Vector Z -0.404759000
MPS Diff
0.851
CSS Angle TLM 1.66389
CSS Sun-Pointing Angle 3.32778
22 Dec 18 @22:00
CSS Angle TLM 1.08336
CSS Sun-Pointing Angle 2.16672
27 Dec 18 @12:00
Pre-Burn
Thruster 1 2880 22 Dec 18 @22:00
Thruster 2 2832
Thruster 3 3280
Thruster 4 3328
Post-Burn
Thruster 1 3312 27 Dec 18 @12:00
Thruster 2 3216
Thruster 3 3696
Thruster 4 3792
Number of Pulses
Thruster 1 432
Thruster 2 384
Thruster 3 416
Thruster 4 464
Thruster Pairs
Thruster 1 & 2 816
Thruster 3 & 4 880
Timothy E. Perry
Mission Operations
CRS, IBEX, OCO-2 & TESS
RAPTOR Test Team
Office (703) 406-5976
Cell (301) 606-1430