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
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.
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
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”.
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
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
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
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 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
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
SOMP Students Oxygen Measurement Project – Image credit Technische Universität Dresden
The Student Oxygen Measurement Project (SOMP) is a cubesat developed by students of the Technische Universität Dresden, Germany, organized in the Students’ Research Group for Spacecraft Engineering in Dresden (STARD). SOMP will be a standard sized single CubeSat (10X10X10 cm) with one payload side and five sides with two solar cells each. The antenna concept foresees a 4 monopole concept. The CubeSat will be able to determine and to a limited extent, also control the attitude.
It is planned to launch on April 19, 2013, from Baikonur in Kazakhstan along with OSSI-1, BEESAT2 and BEESAT3. A variety of downlink options on 437.485 MHz have been proposed, including CW, 1k2 and 9k6 BPSK and AX25 FSK also AO40 standard 400bit/s BPSK
SOMP is an educational satellite project. Designing and developing SOMP will allow the students to practically apply their knowledge and gaining unique hands-on experience in many aspects of a space project. The mission objectives are:
1. Prototype development of a satellite bus
2. Verification of the satellite
3. Launch of the satellite SOMP
4. Establishment of first contact with SOMP
5. Operation of the satellite to fulfill scientific mission objectives
SOMP has two scientific objectives: the first objective is to measure the concentration of atomic oxygen in the upper atmosphere using an oxygen electrolyte sensor. The second is the testing of flexible thin film solar cells (TFSC), that have never been tested in space before.
Contact the SOMP team at stard@mailbox.tu-dresden.de
OSSI-1 is planned to launch April 19, 2013 into a 575 km 63° inclination orbit on a Soyuz-2-1b rocket from the Baikonur launch facility in Kazakhstan along with the Bion-M1 satellite and the SOMP, BEESAT 2, BEESAT 3 and Dove-2 CubeSats. The OSSI VHF beacon is understood to be using 12 WPM CW.
AMSAT-UK 
You must be logged in to post a comment.