AMSAT OSCAR-40 Operations 

 

 

Analogue Operations
US1/2 Transponder Reception

Digital Operations
Telemetry
RUDAK

AO-40 Hardware
AO-40 Spacecraft Antennas
AO-40 K Band Transponder

EA4LE / KC2HAX  AO-40 Equipment
Main Station Antennas
DSS dish and 28 turn helix
Helix feed-horn for 2.4 GHz

AO-40 Deck Receiving System

 

AO-40 Links
AMSAT-DL, AO-40 Status
AMSAT-UK, AO-40 News
AMSAT-NA, AO-40 RUDAK
AO-40 Telemetry info
AO-40 Keplerian elements

JAMSAT, Scope Experiment
AO-40, getting started

 

Favorite Personal Pages
G6LBV Info archive
JF6BCC, Yoshi
K5OE, Antennas

AMSAT Homepages
AMSAT-NA, Homepage
AMSAT-EA, Homepage


US1/2 Transponder Reception


Spacecraft Antennas and Transmitters

                          
                   

AO-40 S Band antennas S1 (left) and S2 (right)

Transponder PEP* (watts) PEP (dBm) Antenna Gain (dBi) PEP S Band (dBm)
S1 38 45.8 18.0 63.8
S2 50 47.0 10.5 57.5
S1 vs. S2       + 6.3 dB

Table. Comparison of the theoretical performance of the S1 and S2 transponder downlink, with the satellite in the same position in space and same transponder load. Based on this comparison signals should be at least 6.3 dB (more than 2 S units) stronger on S1. 

Visit my AO-40 Transmitter antennas page for more details on the S Band (S2) and K Band antennas

CW Tests

Figure. Uplink test from KC2HAX, CW carriers were transmitted in the U band uplink at different power levels from 5 to 50 watts and received on the S2 downlink, chart shows received signal levels compared with the MB Beacon, each division in the chart is ~10dB

 

SSB Tests

 

Mode US1 signals  from AO-40 on the first day of AO-40 Transponder S1 pass-band operation (August, 03, 2001)

 

Ground Station equipment (S Band)

Modified TSI 3733 Receive converter (~1.1 dB NF, 37 db conversion gain) with own dipole at the focus of a Connifer grid dish (~21 dBi), IF receiver is Yaesu FT-847.

Transmitting equipment (U Band) 

Yaesu FT-847(20 Watts), 11 elements linear polarized Yagi antenna (13.2 dBd) EIRP ~240 Watts

Mode US2 signals from S2 transponder at apogee (60000 Km range) before the raise of perigee.

 

Ground Station  equipment (S Band)

Stock TSI 3733 Receive converter (~4.0 dB NF, 37 db conversion gain) with own dipole at the focus of a Connifer grid dish (~21 dBi), IF receiver is Yaesu FT-847.

Transmitting equipment (U Band)

Yaesu FT-847(50 Watts), 11 elements linear polarized Yagi antenna (13.2 dBd) EIRP ~600 Watts

 

Telemetry Reception


Figure. MB Beacon signal on S2 transmitter received at KC2HAX from AO-40 at 57,816 Km range

 

Figure. MB Signal on S2, Chart shows signal to noise ratios as received at KC2HAX, unloaded transponder 

passband (left) and MB Beacon on S2  downlink (right).

 

RUDAK


                

G3RUH 9600bps modem loopback "EYE" Pattern (overdeviated to show EYE details) and RX clock waveform (left). AO-40 RUDAK-A S2 "EYE" pattern received with same modem at KC2HAX (right) 

RUDAK reception performance to date has been outstanding at KC2HAX. On August 08, 2001 at the time the RUDAK team was downloading the first space images form the SCOPE experiment, the signals were here very strong. With RUDAK on the S2 transmitter (no transponder, no MB) signal was steady S 7 (36 dB over noise floor of 1 S unit here). At the time the S1 transmitter was switched on for RUDAK the engineering beacon (EB) was also on (2400.6 MHz), with this configuration the S-meter showed S9+20. These observations are consistent with more than 6dB gain in signal power as the squint was not yet significantly better. Minutes later  the EB was switched off and the RUDAK signal went-up to S9+40dB and peaking at +60 dB !!!!!!! The efficiency meter in WiSP MSPE during the downloading session was showing 100% most of the time.

AO-40 at the time it was Phase 3D, Peter Guelzow, DB2OS and Karl Meinzer, DJ4ZC

Copyright  © 2001 Antonio Fernández, Web Page. AO-40 Photos by Wilfried Gladisch © AMSAT-DL

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