CubeSats with Ham Radio Payloads Deployed

CubeSat deployment pods on top of the Bion-M1 spacecraft BeeSat-2, BeeSat-3 and SOMP are in the three 1U Launchers in the front OSSI-1 is a 1U and alone in a 3U-Pod behind left DOVE-2 is a 3U Cubesat and fills the 3U-Pod behind right

CubeSat deployment pods on top of the Bion-M1 spacecraft
BeeSat-2, BeeSat-3 and SOMP are in the three 1U Launchers in the front
OSSI-1 is a 1U and alone in a 3U-Pod behind left
DOVE-2 is a 3U Cubesat and fills the 3U-Pod behind right

The BeeSat-2, BeeSat-3 and SOMP CubeSats carrying amateur radio payloads were deployed from the Bion-M1 spacecraft on Sunday, April 21.

Signals from BeeSat-2 and SOMP have been received by Mike Rupprecht DK3WN, see

SOMP CW beacon active http://www.dk3wn.info/p/?p=32685

BeeSat-2 CW beacon active http://www.dk3wn.info/p/?p=32683

Satellite        Downlink                Mode
———-       —————          ——————
OSSI-1        145.980/437.525   CW and 1200bps FSK AX.25
SOMP         437.485               1200, 9600bps BPSK
BEESAT-2   435.950               4800bps GMSK Mobitex
BEESAT-3   435.950               4800bps GMSK Mobitex
Bion-M1      Biological research satellite
AIST           Russian student microsatellite that aims to measure the Earth’s geomagnetic field (435 MHz downlink, 145 MHz command uplink)
Dove-2        Commercial technology demonstration mission (450 MHz band downlink)

Further information at https://amsat-uk.org/2013/04/17/soyuz-cubesat-launch/

Keps / TLE’s:

BEESAT-2
1 99999U BEESAT-2 13111.50000000 -.00000022  00000-0 -18943-5 0 00009
2 99999 065.0052 026.5594 0011818 218.6713 261.0081 14.97601851000171
BEESAT-3
1 99998U BEESAT-3 13111.50000000 -.00000022  00000-0 -18943-5 0 00009
2 99998 065.0052 026.5594 0011818 218.6713 261.0081 14.97601851000170

OSSI-1 Amateur Radio CubeSat Launched

Hojun Song DS1SBO performing final assembly of OSSI-1 satellite on April 9, 2013

Hojun Song DS1SBO performing final assembly of OSSI-1 satellite on April 9, 2013

The OSSI-1, BEESAT-2, BEESAT-3 and SOMP amateur radio CubeSats lifted off on a Soyuz-2-1a with research satellites Bion-M1, AIST and Dove-2 from Launch Complex 31 at Baikonur in Kazakhstan on Friday, April 19 at 1000 UT. The OSSI-1 CubeSat was deployed from its Pod on the top of Bion-M1 at 1615 UT.

Soyuz-2-1a Lift-off - Image credit SpaceShuttleAlmanac

Soyuz-2-1a Lift-off – Image credit SpaceShuttleAlmanac

The launch vehicle went into an initial elliptical orbit of 290 km by 575 km orbit at an inclination of 64.9°. A series of orbital maneuvers will be carried out to raise the orbit to 575 km circular before BEESAT-3, SOMP, then BEESAT-2 are deployed at around 1045 UT on Sunday, April 21.

The Center for Operation of Space Ground-Based Infrastructure said the satellites attached to the outer surface of the spacecraft “Bion-M” will be deployed in the period between the 4th and the 35th orbit. It is thought this may mean deployments will take place on the 4th and the 32-34th orbit but that there will be no deployments on the other obits.

OSSI-1 weighs 963 grams

OSSI-1 weighs 963 grams

Korean artist Hojun Song DS1SBO has spent 7 years developing his Open Source Satellite Initiative satellite OSSI-1. He has designed and built it from scratch using readily available components rather than expensive space qualified hardware. The launch was the most expensive part of the project costing $100,000.

It has a 12 WPM CW Morse code beacon on 145.980 MHz, a data communications transceiver on 437.525 MHz using AX.25 packet radio and carries a 44 watt LED optical beacon to flash Morse code messages to observers on Earth.

When deployed the OSSI-1 145.980 MHz Morse Code beacon will send “OS0 DE OSSI1 ANYOUNG”.

Open Source Satellite Initiative blog http://opensat.cc/blog/launch/ossi-1-satellite-launch/

The OSSI telemetry data format spreadsheet can be seen at https://docs.google.com/spreadsheet/ccc?key=0AjtQ6cJ4QOqJdGpHNnRtUWZJV0w4TTFKRU9WYTZqc3c#gid=5

CubeSat deployment pods on top of the Bion-M1 satellite

CubeSat deployment pods on top of the Bion-M1 spacecraft

The development of the OSSI satellite has been documented on the Open Source Satellite Initiative Blog http://opensat.cc/blog/ and the Wiki http://opensat.cc/wiki/

Twitter https://twitter.com/OPENSAT

The Korean national amateur radio society KARL described the OSSI-1 CubeSat in their report to the International Amateur Radio Union Region 3 Triennial conference which was held in Viet Nam in 2012. Read the report at http://www.iaru-r3.org/15r3c/docs/019.doc

In this 20 minute video Korean artist Hojun Song DS1SBO and Donghee Park describe the Open Source Satellite Initiative amateur radio CubeSat OSSI-1.

Watch How OSSI-1 Satellite Works: General Overview

Additional OSSI-1 information at https://amsat-uk.org/satellites/ossi-1/

Watch the BBC TV report: Korean artist has high hopes for his homemade satellite
http://www.bbc.co.uk/news/world-asia-19007475

Hojun Song DS1SBO and the NovaNano FlyMate™ deployer

Hojun Song DS1SBO and the NovaNano FlyMate™ deployer

Satellite        Downlink                Mode
———-       —————          ——————

Russian Student Satellite AIST-2 on BION-M1 launch

Russian Student Satellite AIST-2 on BION-M1

OSSI-1        145.980/437.525   CW and 1200bps FSK AX.25
SOMP         437.485               1200, 9600bps BPSK
BEESAT-2   435.950               4800bps GMSK Mobitex
BEESAT-3   435.950               4800bps GMSK Mobitex
Bion-M1      Biological research satellite
AIST           Russian student microsatellite that aims to measure the Earth’s geomagnetic field
(435 MHz downlink, 145 MHz command uplink)
Dove-2        Commercial technology demonstration mission (450 MHz band downlink)

Predicted Keps / TLE’s:

OSSI-1
1 39130U 00000    13108.66833333  .05491454  00000-0  10000-3 0 00014
2 39130 064.8675 103.2000 0241259 064.9287 214.9800 15.56817350000015

BEESAT-2
1 99999U          13110.41666667 -.00000032  00000-0 -27259-5 0 00006
2 99999 064.9888 015.3126 0011850 230.4664 032.8952 14.97640844000015

Bion-M1 is carrying live mice, geckos and gerbils, see the BBC story at http://www.bbc.co.uk/newsround/22218589

Space News Feed http://www.spacenewsfeed.co.uk/index.php/launches/14433-bion-m-1-aist-2-beesat-2-beesat-3-dove-2-ossi-1-somp

Soyuz-2-1a Bion-M1 Launch

Soyuz-2-1a Bion-M1 Launch – Image credit SpaceShuttleAlmanac

Soyuz Ham Radio CubeSat Launch

CubeSat deployment pods on top of the Bion-M1 spacecraft

CubeSat deployment pods on top of the Bion-M1 spacecraft
BeeSat-2, BeeSat-3 and SOMP are in the three 1U Launchers in the front
OSSI-1 is a 1U and alone in a 3U-Pod behind left
DOVE-2 is a 3U Cubesat and fills the 3U-Pod behind right

Soyuz-2-1a is planned to launch Friday, April 19, 2013 at 1000 UT from Baikonur in Kazakhstan. Among the satellites it will carry are four CubeSats with amateur radio payloads, OSSI-1, BEESAT-2, BEESAT-3 and SOMP.

Unusually the CubeSats will not be deployed straight after launch. Deployment of OSSI-1 is expected to take place after the 4th orbit and BEESAT-3, SOMP then BEESAT-2 are expected to be deployed at 16 second intervals after the 32nd orbit on Sunday, April 21 at around 1045 UT. Until then orbital maneuvers will be carried out to achieve a circular orbit at 575 km altitude.

It is expected that the four CubeSats may be deployed at intervals of about 16 seconds.

The satellites on the launch are:

Bion-M1
Bion-M is the next generation of Russian biological research satellites. While retaining the Vostok/Zenit-derived reentry module of the earlier Bion, the propulsion module has been replace by a Yantar type module, which provides maneuvering capabilities and longer mission support. The mission duration has been increased to up to 6 months by using solar cells for energy generation. The weight of scientific equipment has been increased by 100 kilograms. Source Gunters Space Page
Bion-M1 is carrying live mice, geckos and gerbils, see the BBC story at http://www.bbc.co.uk/newsround/22218589

Watch Bion-M Mission

Russian Student Satellite AIST-2 on BION-M1 launch

Student Satellite AIST-2

AIST-2
AIST is a russian microsatellite developed by designed by a group of students, postgraduates and scientists of Samara Aerospace University in cooperation with TsSKB Progress.

The satellite will measure the geomagnetic field, test the new small space vehicle bus, test methods to decrease microaccelerations to a minimum level and measure micrometeoroids of natural and artificial origin. Source Gunters Space Page
Believed to have a 435 MHz downlink and an 145 MHz command uplink.

OSSI-1 weighs 963 grams

OSSI-1 weighs 963 grams

OSSI-1
Korean artist Hojun Song DS1SBO has spent 7 years developing his Open Source Satellite Initiative satellite OSSI-1. He has designed and built it from scratch using readily available components rather than expensive space qualified hardware.

It has a 12 WPM CW Morse code beacon on 145.980 MHz, a data communications transceiver on 437.525 MHz and carries a 44 watt LED optical beacon to flash Morse code messages to observers on Earth.
https://amsat-uk.org/satellites/ossi-1/

BEESAT-1 Engineering Qualification Model

BEESAT-1 Engineering Qualification Model

BEESAT 2
The Berlin Experimental and Educational Satellite 2 is a 1U CubeSat project intended to test a reaction wheel and an Attitude Determination and Control (ADC) system. It will also carry an experimental camera.
http://tinyurl.com/TUB-BEESAT

BEESAT 3
A 1U CubeSat project intended to test a transmitter using commercial S Band frequencies outside the amateur satellite service but will have a downlink on 435.950. It will have passive attitude control.
http://tinyurl.com/TUB-BEESAT

SOMP-1SOMP
The Student Oxygen Measurement Project (SOMP) is a 1U cubesat developed by students of the Technische Universität Dresden, Germany, organized in the Students’ Research Group for Spacecraft Engineering in Dresden (STARD). The CubeSat will be able to determine and to a limited extent, also control the attitude
https://amsat-uk.org/2013/03/22/somp-students-oxygen-measurement-project-carries-amateur-radio-payload/

Dove-2
The Dove-2 mission is a technology demonstration nanosatellite for Cosmogia Inc. for remote sensing purposes based on the triple (3U) CubeSat form factor. It is also an internal company technology demonstration experiment to test the capabilities of a low-cost spacecraft constrained to the 3U cubesat form factor to host a small payload. Dove 2 is licensed to collect images of the Earth and will undertake a short-duration experimental mission in a 290 km by 575 km orbit at an inclination of 64.9°.
Source Gunters Space Page

It is believed Dove-2 will have a downlink in the 450 MHz band. Search for Cosmogia at https://apps.fcc.gov/oetcf/els/reports/GenericSearch.cfm

Satellite        Downlink                Mode
———-       —————          ——————
OSSI-1        145.980/437.525   CW and 1200bps FSK AX.25
SOMP         437.485               1200, 9600bps BPSK
BEESAT-2   435.950               4800bps GMSK Mobitex
BEESAT-3   435.950               4800bps GMSK Mobitex
Bion-M1      Biological research satellite
AIST           Russian student microsatellite that aims to measure the Earth’s geomagnetic field (435 MHz downlink, 145 MHz command uplink)
Dove-2        Commercial technology demonstration mission (450 MHz band downlink)

Predicted Keps / TLE’s:

BEESAT-2
1 99999U          13110.41666667 -.00000032  00000-0 -27259-5 0 00006
2 99999 064.9888 015.3126 0011850 230.4664 032.8952 14.97640844000015

Space News Feed http://www.spacenewsfeed.co.uk/index.php/launches/14433-bion-m-1-aist-2-beesat-2-beesat-3-dove-2-ossi-1-somp

Student CubeSats BEESAT-2 and BEESAT-3

BEESAT-1 Engineering Qualification Model

BEESAT-1 Engineering Qualification Model

Two CubeSats, built by students at the Technical University of Berlin, are expected to launch in the 4th quarter of 2012 from Baikonour into a 575km circular 65 degree orbit.

BEESAT-2 is a 1U cubesat project intended to test a reaction wheel and an Attitude Determination and Control (ADC) system. Will also carry an experimental camera.

BEESAT-3 is a 1U cubesat project intended to test a transmitter using commercial S Band frequencies outside the amateur satellite service.

Up- and downlink of both of these CubeSats is established by half-duplex GMSK modulated narrow-band radio at 436.000 MHz. The standard data rate is 4800 bps but can be switched to 9800 bps for increased channel capacity at higher elevations. Each transmission at the higher data rate is announced by a small 4800 bps header to allow for adaptive receiver re-configuration. The modem device used is the CML CMX909b.

For more information see http://tinyurl.com/TUB-BEESAT

IARU Amateur Satellite Frequency Coordination pages hosted by AMSAT-UK http://www.amsat.org.uk/iaru/