baalke@mars.jpl.nasa.gov (Ron Baalke) (11/10/90)
Voyager Status Report November 9, 1990 Voyager 1 The Voyager 1 spacecraft collected routine UVS (Utraviolet Spectrometer) data on source SS CYGNI. On October 29, one frame of high-rate PWS (Plasma Wave) was recorded. On November 1, there was a slew to a position pointing toward Voyager 2 to observe interstellar hydrogen levels between the two spacecraft. On October 30 a DTR (Digital Tape Recorder) Maintenance sequence was executed. The X Band TWT (Traveling Wave Tube) was also commanded to the high power mode and the Bay 1 heater was turned off in preparation for Playback #4. On October 31 Playback # 4, containing PWS data, was executed; DSN (Deep Space Network) performance for the playback was nominal. Following the playback, the X Band TWT was returned to the low power mode and Bay 1 heater turned on. A TLC (Tracking Loop Capacitor) test was also performed by the Goldstone 34 meter station. On November 1, real-time commands to reset the CCS (Computer Command Subsystem) Status Telemetry, change the FDS (Flight Data Subsystem) data mode, load the AACS (Attitude and Articulation Control Subsyste) and CCS Memory readout mini-sequence for execution on November 2, load the AACS software fix (Gyro Drift Turn), Reset the Command Loss Timer, perform a CCSTIM (CCS Timing) Test, perform a CCSCAL (CCS Calibration) Test, and return the FDS to its original mode, were transmitted to the spacecraft. Many problems were experienced while attempting to command which caused all but the first command to be delayed, and some to be transmitted out of the planned order. The second element of the CCS Status Telemetry Reset command was aborted at the first attempt and was not retransmitted as it was redundant. Delays from one hour and twenty five minutes to four hours and forty seven minutes were experienced in the command file transmission. All transmitted commands were eventually successfully received by the spacecraft and executed; CCS checksum verification was received. The CCSTIM and CCSCAL tests were executed and analysis indicates there has been no change in the time offset between the FDS frame start and the CCS timing chain in each CCS processor nor in the CCS instruction cycle timing when compared with the sequence timing derived from the FDS oscillator. Voyager 2 The Voyager 2 spacecraft collected UVS background in the anti-Voyager 1 direction. On November 1, the scan platform was slewed to point towards Voyager 1 to observe interstellar hydrogen levels between the two spacecraft. Background levels will be removed by subtracting out the data from when the spacecraft were pointed away from each other. On October 30, one frame of high-rate PWS data was recorded. CONSUMABLE STATUS AS OF 11/9/90 P R O P E L L A N T S T A T U S P O W E R Consumption One Week Propellant Remaining Output Margin Spacecraft (Gm) (Kg) Watts Watts Voyager 1 5 36.3 + 2.0 367 55 Voyager 2 6 39.3 + 2.0 370 61 ___ _____ ___ /_ /| /____/ \ /_ /| | | | | __ \ /| | | | Ron Baalke | baalke@mars.jpl.nasa.gov ___| | | | |__) |/ | | |___ Jet Propulsion Lab | baalke@jems.jpl.nasa.gov /___| | | | ___/ | |/__ /| M/S 301-355 | |_____|/ |_|/ |_____|/ Pasadena, CA 91109 |
wayne@csri.toronto.edu (Wayne Hayes) (11/11/90)
In article <1990Nov10.001052.28690@jato.jpl.nasa.gov> baalke@mars.jpl.nasa.gov (Ron Baalke) writes: > Voyager 1 > On November 1, there was a slew to a position pointing >toward Voyager 2 to observe interstellar hydrogen levels between the two >spacecraft. > Voyager 2 > The Voyager 2 spacecraft collected UVS background in the anti-Voyager 1 >direction. On November 1, the scan platform was slewed to point towards >Voyager 1 to observe interstellar hydrogen levels between the two spacecraft. >Background levels will be removed by subtracting out the data from when the >spacecraft were pointed away from each other. Does this mean that they beamed some radio waves at each other to measure the absorbance at 21.1 cm? Do the spacecraft actually have powerful enough transmitters and sensitive enough receivers to actually detect each other? Or is it something to do with the absorbancy/emmission seen in all directions, and we're trying to measure a teensy-weensy delta between the background measured by spacecraft X minus the same background from the same direction measured by spacecraft Y? -- "Dad, what should I be when I grow up?" "Honest." -- Robert M. Pirsig, _Zen and the Art of Motorcycle Maintenence_. Wayne Hayes INTERNET: wayne@csri.utoronto.ca CompuServe: 72401,3525