Live tracking
Day 60 update: 26-Apr-2020 (Final, RIP)
Day 59 update: 25-Apr-2020
Day 58 update: 24-Apr-2020
Day 57 update: 23-Apr-2020
Day 56 update: 22-Apr-2020
Day 55 update: 21-Apr-2020
Day 54 update: 20-Apr-2020
Day 53 update: 19-Apr-2020
Day 52 update: 18-Apr-2020
Day 51 update: 17-Apr-2020
Day 50 update: 16-Apr-2020
Lap three updates
Lap two updates
Lap one updates
Launch photos
Transmitter
This is the 2nd test flight of the new U4B tracker. For details see below.
U4B-2 was launched by Dave VE3KCL on 01-Mar-2020 early in the morning (1210Z). The transmitter callsign is VE3KCL and telemetry channel 04 (in the old system way of looking at things). Transmissions are on 20m only. Standard WSPR transmission at :08, :18, :28 etc past the hour, followed by the telemetry packet at :10, :20, :30 etc.
Live tracking
Day 60: 26-Apr-2020 (Final, RIP)
There was no Day 60... overnight on 25-Apr-2020 to 26-Apr-2020 U4B-2 came down. Run out of gas, presumably. There are clues in the altitude plot, see below, this is an extract of the altitude data, for the last 7 days of flight. Some altitude change is normal. But you can see a distinct trend in altitude loss right there on the last day.
RIP, U4B-2, that was an AWESOMELY great flight. AWESOMENESS overload. 1 month, 24 days. 124,000 km. And 3.5 laps around the planet Earth.
DOWNLOAD of the Excel complete data set for this flight, CLICK HERE.
Day 59: 25-Apr-2020
Day 58: 24-Apr-2020
Day 57: 23-Apr-2020
Day 56: 22-Apr-2020
Day 55: 21-Apr-2020
Day 54: 20-Apr-2020
Day 53: 19-Apr-2020
Day 52: 18-Apr-2020
Day 51: 17-Apr-2020
Day 50: 16-Apr-2020
Day 49: 15-Apr-2020
U4B-2 completed circumnavigation number 3!
Day 48: 14-Apr-2020 (again)
Day 47: 14-Apr-2020
Day 46: 13-Apr-2020
Day 45: 12-Apr-2020
Day 44: 11-Apr-2020
Day 43: 10-Apr-2020
Day 42: 09-Apr-2020
Day 41: 08-Apr-2020
Day 40: 07-Apr-2020
Day 39: 06-Apr-2020
Day 38: 05-Apr-2020
Day 36: 03-Apr-2020
Day 35: 02-Apr-2020
Day 33: 31-Mar-2020
Day 32: 30-Mar-2020
Day 31: 29-Mar-2020
Second circumnavigation completed!
Day 30: 28-Mar-2020
Day 29: 27-Mar-2020 (again)
Day 28: 27-Mar-2020
Day 27: 26-Mar-2020
Day 26: 25-Mar-2020
Day 25: 24-Mar-2020
Day 24: 23-Mar-2020
Day 23: 22-Mar-2020
Day 22: 21-Mar-2020
Day 21: 20-Mar-2020
Day 20: 19-Mar-2020
Day 19: 18-Mar-2020
Day 18: 17-Mar-2020
Day 17: 16-Mar-2020
Day 16: 15-Mar-2020
Circumnavigation completed, a complete lap of planet Earth!
Day 15: 14-Mar-2020
Day 14: 13-Mar-2020
Day 13: 12-Mar-2020
Yes... 12th March AGAIN... because U4B-2 passes the international date line.
Day 12: 12-Mar-2020
Day 11: 11-Mar-2020
Day 10: 10-Mar-2020
Day 9: 09-Mar-2020
Day 8: 08-Mar-2020
Day 7: 07-Mar-2020
Day 6: 06-Mar-2020
Day 5: 05-Mar-2020
The map (below left) shows reception reports of U4B-2 during the last 3 hours of operation today.
Day 4: 04-Mar-2020
Day 3: 03-Mar-2020
Great excitement here at QRP Labs HQ today, when I got my 20m WSPR receiver dusted off and back in action after almost a year on the shelf. I was happy to record 14 reports as U4B-2 rushed across France and over the Mediterranean, and a smaller number of telemetry reports too. This is a list of the standard WSPR transmission reports:
Power Reported Distance
Date Call Frequency SNR Drift Grid dBm W by loc km mi
2020-03-03 16:28 VE3KCL 14.097196 -29 0 JN40 +10 0.010 TA4/G0UPL KM46 1793 1114 2020-03-03 15:48 VE3KCL 14.097195 -25 -1 JN41 +10 0.010 TA4/G0UPL KM46 1811 1125 2020-03-03 15:18 VE3KCL 14.097198 -29 -1 JN41 +10 0.010 TA4/G0UPL KM46 1811 1125 2020-03-03 14:48 VE3KCL 14.097198 -28 0 JN41 +10 0.010 TA4/G0UPL KM46 1811 1125 2020-03-03 14:28 VE3KCL 14.097198 -25 -1 JN31 +10 0.010 TA4/G0UPL KM46 1975 1227 2020-03-03 14:18 VE3KCL 14.097197 -25 0 JN32 +10 0.010 TA4/G0UPL KM46 1996 1240 2020-03-03 14:08 VE3KCL 14.097196 -26 0 JN32 +10 0.010 TA4/G0UPL KM46 1996 1240 2020-03-03 13:38 VE3KCL 14.097195 -23 0 JN32 +10 0.010 TA4/G0UPL KM46 1996 1240 2020-03-03 13:18 VE3KCL 14.097195 -25 0 JN32 +10 0.010 TA4/G0UPL KM46 1996 1240 2020-03-03 12:48 VE3KCL 14.097203 -24 0 JN22 +10 0.010 TA4/G0UPL KM46 2157 1340 2020-03-03 12:38 VE3KCL 14.097202 -27 0 JN22 +10 0.010 TA4/G0UPL KM46 2157 1340 2020-03-03 12:28 VE3KCL 14.097202 -29 0 JN22 +10 0.010 TA4/G0UPL KM46 2157 1340 2020-03-03 11:58 VE3KCL 14.097202 -27 0 JN23 +10 0.010 TA4/G0UPL KM46 2179 1354 2020-03-03 11:38 VE3KCL 14.097203 -25 0 JN23 +10 0.010 TA4/G0UPL KM46 2179 1354
The receiver is built using two QRP Labs kits:
- Receiver module kit http://qrp-labs.com/receiver built for 20m
- ProgRock module kit http://qrp-labs.com/progrock as the LO.
These two modules are mounted in an aluminium enclosure and powered at 12V using my homebrew linear-regulated radio PSU. Antenna is my OCFD. Along with those modules there's also:
- 7805 voltage regulator to produce +5V DC for the modules
- Some L-C filters (random junkbox chokes and electrolytic capacitors) to filter the DC some more
- On/Off switch and Power LED
- 12dB and 6dB attenuators which can be switched in or out, providing 0, 6dB, 12dB or 18dB of RF attenuation
- Multi-turn trimmer potentiometer to set the audio level
- 3.5mm stereo jack for audio output
- 3.5mm mono jack where I can connect 1pps from my QLG1 GPS Receiver kit http://qrp-labs.com/qlg1 to calibrate the oscillator reference.
Some photos below:
U4B-2 continued transmitting until long after dark, the final transmission showed a temperature of -39C and battery voltage of 2.39V, but it was still getting reports! Note that the temperature may not be reliable since the supply voltage is below the specified voltage for the LM temperature sensor; and below 2.7V the GPS module isn't able to provide a position fix either.
Day 2: 02-Mar-2020
Day 1: 01-Mar-2020
Launch photos
Transmitter
This is the 2nd test flight of the new U4B tracker. U4B-2 was assembled by Dave VE3KCL. This YouTube video explains the features of the U4B tracker.
The U4B-2 flight features a change in the firmware, which allows the Si5351A Synthesizer to drive the two sides of the dipole in anti-phase, rather than just one side against ground in previous flights. The result is a 3dB increase in output power. High or low power can be controlled also via the BASIC program; for the time being, the I variable is used to control whether high power (I = 1) or low power (I = 0) is used. In this flight, high power is used if the battery voltage is above 3.8V. When the battery voltage falls below 3.8V the system is switched to low power by setting I = 0.
The BASIC program listing:
5 LET C = 41 10 PRINT BT 11 IF BT < 3200 12 SLEEP 10 1 13 GOTO 10 14 ENDIF 15 LET FR = 27000001 20 OUT 9 0 25 GPS 300 "$PSIMNAV,W,3*3A" 26 OUT 9 CL 28 SLEEP 10 7 30 PRINT BT 32 IF BT > 3800 33 LET I = 1 34 GOTO 40 38 ENDIF 39 LET I = 0 40 CW 0 14097235 12 0 "_VE3KCL" 45 CW 2 14097235 4 10 "TT" 55 TELE 60 GOTO 15
Photos