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Photo of AMSAT OSCAR 16


Spacecraft Summary

OSCAR Designation:  AMSAT OSCAR 16     Oscar Number:  AO-16    
International Designator:  1990-005D     Norad Number:  20439    
Common Name:  PacSAT     Satellite Type:  Microsatellite    
Launch Date:  22 January, 1990     Launch Location:  French Guiana    
Launch Vehicle:  Ariane 4     Apogee:  794.00    
Perigee:  778.00     Inclination:  98.19    
Period:  100.58     Dimensions:  22.6 x 22.6 x 22.3 cm
Weight:  13.340 Kg    
Organization: AMSAT-NA

Frequency Information
Mode V/U (J) PacSat BBS: Non-Operational
Downlink 437.0260 MHz BPSK 1200 BPS
Downlink 437.0510 MHz BPSK 1200 BPS
Uplink: 145.9000 MHz MFSK 1200 BPS
Uplink: 145.9200 MHz MFSK 1200 BPS
Uplink: 145.9400 MHz MFSK 1200 BPS
Uplink: 145.9600 MHz MFSK 1200 BPS
Mode S Packet: Non-Operational
Downlink 2401.1428 MHz BPSK 1200 BPS
Mode FM Voice Repeater (Downlink is DSB. Operation is Intermittent): Semi-Operational
Simplex: 145.9200 MHz FM
Downlink 437.0260 MHz SSB/CW

Current Keplerian Elements

1 20439U 90005D   11059.92250183  .00000033  00000-0  28056-4 0  1294
2 20439  98.3706  13.2330 0011537 121.4401 238.7912 14.31897436102129

Detailed Description

Based on the success of UoSAT-OSCAR-11's Digital Communications Experiment, AMSAT-OSCAR-16 was designed to be a dedicated store-and-forward file server in space. Using 1200 bit per second Mode JD radio links, AMSAT-OSCAR-16 interacts with ground station terminal software to appear as a packet radio bulletin board system to the user. Anyone wishing to download files, personal mail from anywhere in the world, or news bulletins could request the information be "broadcast" to all under the footprint of the spacecraft, or directed specifically to that ground station. This broadcast protocol differs from terrestrial packet radio communications, but allows a greater number of ground stations access to the spacecraft's resources during the limited time of a pass.

A total of 10 megabytes of static RAM was used for message storage and a RAM disk. PACSAT communicated with ground stations through a single downlink channel and a total of four uplink channels. The multi-tasking operating system allows mailbox software and an AX.25 protocol driver to operate concurrently.

Only one 70-cm downlink transmitter is active at any one time. Due to performance degradation of the primary transmitter on 437.026 MHz, the secondary transmitter on 437.051 MHz is being used at the current time. All Microsats transmit using several watts of transmitter power making their signals easily received on the Earth below. AMSAT-OSCAR-16 accepts 1200 bps 3.5 KHz deviation Manchester encoded FSK on any of its uplink frequencies. It transmits using 1200 bps binary phase shift keying (BPSK), a very robust binary modulation scheme.

AO-16 uplinks are made with 2-Meter FM voice transmitters, while downlink reception requires a 70-cm SSB receiver or HF SSB receiver with a 70-cm converter. Several modem designs are available for Pacsat operation. These modems are also mode compatible with Fuji-OSCAR-20.

The uplink receivers are VERY sensitive. AX.25 connection to the spacecraft can be made with just a few watts of transmitter power and a modest antenna system. While testing a newly designed 1200 bps Pacsat modem, it was discovered that seven watts of transmitter power and an indoor antenna were all that was required to connect to oneself using AO-16 as a digipeater.

"Experimenter Days" were scheduled for PACSAT from time to time. During these periods, ground stations were encouraged to limit their uplink transmitter power to the minimum necessary to establish and maintain AX.25 connection with the digital transponder. Usually the transmitter power level was on the order of just a few watts.

Whole Orbit Data (WOD) collections was also performed by AO-16, and WOD files were available through the mailbox for all those who were interested in processing and analyzing spacecraft telemetry.

Reference Documents:

  • D. Conners, "The PACSAT Project,"ARRL Amateur Radio Second Computer Networking Conference, pp. 1-3, March 19, 1983.
  • T. Clark, "AMSAT's Microsat/Pacsat Program,"Proceedings of the AMSAT-NA Sixth Space Symposium, Atlanta, GA, pp. 41-47, Nov 1988, ARRL.
  • L. Johnson and C. Green, "Microsat Project - Flight CPU Hardware,"Proceedings of the AMSAT-NA Sixth Space Symposium, Atlanta, GA, pp. 104-106, Nov 1988, ARRL.
  • H. Price and R. McGwier, "PACSAT Software,"Proceedings of the AMSAT-NA Sixth Space Symposium, Atlanta, GA, pp. 145-149, Nov 1988, ARRL.
  • T. Clark, C. Duncan, J. King, B. McGwier, "The First Flock of Microsats,"The AMSAT Journal, May 1989, pp 3-10.
  • D. Loughmiller and B. McGwier, "Microsat: The Next Generation of OSCAR Satellites," Part 1,QST, May 1989, pp 37-40; Part 2,QST, Jun 1989, pp 53-54.
  • Doug Loughmiller, "Successful OSCAR Launch Ushers in the 90's,"QST, Apr 1990, p. 52.
  • Six for the Price of One - Part I,"The AMSAT Journal, Vol. 13, No. 1, Mar 1990, p. 1; Part II:The AMSAT Journal, Vol. 13, No. 2, May 1990, p. 1.
  • John A. Magliacane, "Spotlight On: The Microsats,"The AMSAT Journal, Vol. 15, No. 4, Sep/Oct 1992
  • Martin Davidoff,The Satellite Experimenter's Handbook, 2nd edition, The American Radio Relay League, Newington, CT., 1990.
  • Mike Crisler,PACSAT Beginner's Guide, AMSAT.

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