PACSAT and LUSAT are two MicroSatellites
that were launched along with other satellites from Kourou, French Guiana, South America. An
Ariane vehicle of the European Space Agency carried the satellites aloft on February 22, 1990 to a
low altitude, sun-synchronous, near polar orbit. Each satellite takes a little more than an
hour and a half to circle the earth at an altitude of nearly 500 miles. Midday, you'll find the
satellites passing north-to-south over the continental United States, and in late evening, the
satellites will pass overhead traveling in the opposite direction.
The satellites are amazingly small. They're
cubed shaped, and approximately nine (9) inches on edge. In fact, the 145 MHz. receive antenna is
twice the length of the main body of the spacecraft. This single element 1/4 wave antenna is
located on the top (+Z surface) of the structure, and the four (4) shorter 437 MHz. transmit
antennas are located on the bottom (-Z surface). All the antennas are made of flexible metal
much like the curved tape measures used by carpenters.
Attitude stabilization and control is maintained by
four (4) small permanent magnets aligned top-to-bottom. With this configuration, the
satellite rotates end-over-end twice per orbit as it tries to align with the earth's magnetic
field. To reduce temperature variations on internal hardware, the spacecraft slowly spins.
This is accomplished by the 145 MHz. antenna acting as a radiometer. One side of the antenna
is painted white and the other black. Solar radiation pressure then causes the craft to
spin.
Each spacecraft is powered by eight (8) NiCd
batteries. The batteries are charged by 440 small solar cells mounted on all surfaces of the
structure. The 22 volt battery bus is converted to 10, 8.5 and 5 volts DC. The CPU is an NEC
V40. 2K of ROM is used for restart and approximately 10.5M of static RAM is used for storage
and the operating system.
PACSAT and LUSAT have been designed to provide AX.25
packet communications in the form of an orbiting mailbox where messages are up-linked, stored and
then forwarded to other Amateur Radio Operators anywhere on the planet. Each satellite has
the capability of receiving on four different frequencies simultaneously in the 145 MHz.
band. Ground stations transmit on one of these frequencies using Manchester encoded FM at +/-
3 kHz. deviation. All ground stations listen to one down link frequency near 437 MHz. using a
single-sideband receiver and a special PSK modem. Communications is full duplex.
Special software is required to handle the protocols
used with this form of satellite communications. The software must be capable of using
Broadcast and FTL0 protocols. PG, PB and Wisp are a few of the programs available. This
software can also be used to download telemetry files generated every minute or so. These
broadcasts give a snapshot of how the spacecraft is functioning. An example of a typical
telemetry download is shown below. Note references to battery voltages and array charge
currents. By looking at the charge current number, you can actually tell which side of the
spacecraft is facing the sun.
57 Sample peg counts follow:
-
0 Rx D DISC: 0.0322
-
1 Rx D S meter: 147
-
2 Rx C DISC: -1.21124
-
3 Rx C S meter:122
-
4 Rx B DISC: -0.06156
-
5 Rx B S meter: 158
-
6 Rx A DISC: 2.4638
-
7 Rx A S meter: 116
-
8 Rx E/F DISC: 3.48286
-
9 Rx E/F S meter: 156
-
10 +5 Volt Bus: 4.9715
-
11 +5V Rx Current: 44.25
-
12 +2.5V VREF: 2.5056
-
13 +8.5V BUS: 8.6802
-
14 IR Detector: 65
-
15 LO Monitor I: 1.702
-
16 +10V Bus: 11.15
-
17 GASFET Bias I: 3.354
-
18 Ground REF: 0
-
19 +Z Array V: 21.483
-
20 +X (RX) Temp: 9.0748
-
21 Rx Temp: -3.0272
-
22 Bat 1 V: 1.35073
-
23 Bat 2 V: 1.397876
-
24 Bat 3 V: 1.3827
-
25 Bat 4 V: 1.319436
-
26 Bat 5 V: 1.369296
-
27 Bat 6 V: 1.48822
-
28 Bat 7 V: 1.398493
-
29 Bat 8 V: 1.38185
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-
30 Array V: 20.4128
-
31 +5V Bus: 6.750977
-
32 +8.5V Bus: 9.331578
-
33 +10V Bus: 11.03501
-
34 BCR Set Point: 137.016
-
35 BCR Load Cur: 320.46
-
36 +8.5V Bus Cur: 25.924
-
37 +5V Bus Cur: 210.08
-
38 -X Array Cur: 106.69
-
39 +X Array Cur: -3.38
-
40 -Y Array Cur: -11.28
-
41 +Y Array Cur: 0.03
-
42 -Z Array Cur: -2.41
-
43 +Z Array Cur: 221.28
-
44 Ext Power Cur: -17.5
-
45 BCR Input Cur: 371.05
-
46 BCR Output Cur: -12.6133
-
47 Bat 1 Temp: 1.8136
-
48 Bat 2 Temp: 1.2085
-
49 Baseplt Temp: 3.0238
-
50 PSK TX RF Out: -0.0290131
-
51 RC PSK TX Out: 0.098498
-
52 RC PSK BP Temp: 4.234
-
53 RC PSK HPA Tmp: 3.0238
-
54 +Y Array Temp: -2.4221
-
55 PSK TX HPA Tmp: 2.4187
-
56 +Z Array Temp: 20.5717
-
57 S band HPA Tmp: 214
-
58 S band TX Out: -0.08365
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This has been a very brief description of two micro-satellites used by Amateur Radio Operators
around the world. For more information about the Amateur Satellite Service, visit AMSAT.
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