SPROUT Slow Scan TV and Digitalker Active

SSTV image received from SPROUT by Mario LU4EOU on May 31, 2014 at 0408 UT

SSTV image received from SPROUT by Mario LU4EOU on May 31, 2014 at 0408 UT

Slow Scan TV (SSTV) images in Scottie 1 format have been successfully received from the amateur radio satellite SPROUT on 437.600 MHz FM (+/- 9 kHz Doppler shift). The Digitalker has also been active.

SPROUT, a 20 x 20 x 22 cm amateur radio nano-satellite with a mass of 7.1 kg, launched successfully with the L-band (1236.5 MHz/1257.5 MHz/1278.5 MHz) Synthetic Aperture Radar (SAR) satellite ALOS-2 on May 24, 2014 at 0305 UT. SPROUT is now in a 654 km, 97.9 degree inclination Sun Synchronous Orbit (SSO).

SPROUT (Space Research On Unique Technology) was built by students from Nihon University and its objectives are:

SPROUT Satellite - Credit Nihon-Univ. Miyazaki Laboratory

SPROUT Satellite – Credit Nihon-Univ. Miyazaki Laboratory

1. Operation of satellite by radio amateurs.

A FM Digitalker will enable the satellite to speak to amateurs around the world.

The Voice Message Box will record transmissions from radio amateurs and play them back.

Pre-loaded images from the Message Gallery can be transmitted using Slow Scan TV (SSTV).

Pictures of the Earth can be transmitted by SSTV and radio amateurs can receive it using free software such as MMSSTV. As part of the Earth mapping project the team ask radio amateurs to contribute pictures they have received from the satellite for display on the SPROUT website.

The satellite also has a packet radio Digipeater and Text Message Box function.

SPROUT in orbit2. Demonstration of the deployment of the combined membrane structure and verification of the design method of the structure SPROUT has a triangular membrane supported by two tubes like framework. They are folded and stored in the satellite before the launch. After the launch, the nitrogen gas is injected into the tubes in space, and they extend, so that the membrane deploys (called “combined membrane structure”).

3. Demonstration of attitude determination and control of a nanosatellite using the sun sensors, gyros, geomagnetic sensor and magnetic torquers.

Callsign: JQ1ZJQ
Size: 214x210x220 mm
Weight: 7.1 kg
Mode: 1200bps AFSK, 9600bps GMSK
CW downlink 437.525 MHz
FM packet downlink 437.525 MHz
Digipeater uplink 437.600 MHz
Digitalker downlink 437.600 MHz
SSTV downlink 437.600 MHz

SPROUT Amateur Radio SSTV Satellite

SPROUT Amateur Radio SSTV Satellite

SPROUT English website http://sat.aero.cst.nihon-u.ac.jp/sprout-e/

SPROUT Japanese website http://sat.aero.cst.nihon-u.ac.jp/sprout/

Nihon-Univ. Miyazaki Laboratory on Facebook
https://www.facebook.com/pages/Nihon-Univ-Miyazaki-Laboratory/406566642818860

Telemetry Software http://sat.aero.cst.nihon-u.ac.jp/sprout-e/2-Software-e.html

Telemetry format http://sat.aero.cst.nihon-u.ac.jp/sprout-e/2-Formats%20of%20telemetry-e.html

SPROUT launch data page
http://sat.aero.cst.nihon-u.ac.jp/sprout-e/2-Launch%20data-e.htmlTLE’s from the North American Aerospace Defence Command (NORAD) are also available at http://celestrak.com/NORAD/elements/tle-new.txt

Adding new satellites to SatPC32, Gpredict and Nova
https://amsat-uk.org/2013/11/23/adding-new-satellites-to-satpc32/

Free Slow Scan TV (SSTV) software MMSSTV http://hamsoft.ca/pages/mmsstv.php

The JE9PEL website has information on other satellites on this launch
http://www.ne.jp/asahi/hamradio/je9pel/jaxalos2.htm

Read the Overview of the L-band SAR Onboard ALOS-2 here.

SPROUT satellite students at Nihon-Univ. Miyazaki Laboratory

SPROUT satellite students at Nihon-University Miyazaki Laboratory

KLETSkous Linear Transponder Demonstration

KLETSkous LogoThis video shows a demonstration, given on May 24, 2014, of the KLETSkous 1U Cubesat amateur radio transponder.

A 435/145 Linear transponder is planned with a bandwidth of 20 kHz.

Currently the team are considering frequencies in the 435.100 to 435.140 MHz range for the uplink and 145.860 to 145.980 MHz for the downlink.

The scientific payload will be an experiment analysing “Worm Holes”. This experiment will try and find the portholes between Sun and Earth.

Further information at http://zr6aic.blogspot.co.uk/search/label/KLETSkous
and at http://www.amsatsa.org.za/

Watch KLETSkous 1U CubeSat Satellite Transponder Demo

GEO 2014 Symposium Videos Released

National Space Centre Leicester

National Space Centre Leicester

A video collection of the presentations given at the Group for Earth Observation (GEO) Symposium on Saturday, April 26, 2014 has been released.

GEO is a group of enthusiasts interested in the amateur reception of weather and earth imaging satellites. They produce a first-rate quarterly magazine, samples can be seen at http://www.geo-web.org.uk/samples.php

Watch the GEO 2014 Symposium videos recorded at the National Space Centre in Leicester at
http://www.geo-web.org.uk/symposium.php

The GEO Yahoo Group can be found at http://groups.yahoo.com/group/GEO-Subscribers/

Group for Earth Observation (GEO)
http://www.geo-web.org.uk/

Manchester: Synergy-Space Meetup

Sotira Trifourki Synergy-SpaceOrganizer Sotira Trifourki reports on the planned Synergy-Space Meetups in the Manchester area.

She says: We are putting together a regular meetup group to start making the CubeSats and Space Telescope’s for our forthcoming missions to the Moon with Team SYNERGY MOON, you can find us here:
http://www.meetup.com/Synergy-Space/

Synergy Moon http://www.synergymoon.com/

TshepisoSAT / ZACUBE-1, six months on orbit

ZACUBE-1, FUNcube-1 and HiNCube in the deployment pod - Image credit Wouter Weggelaar PA3WEG

ZACUBE-1, FUNcube-1 and HiNCube in the deployment pod – Image credit Wouter Weggelaar PA3WEG

The South African CPUT TshepisoSAT team were invited to give a mission update at the SA AMSAT‘s Space Symposium on Saturday, May 24, 2014 at the Innovation Hub in Pretoria.

The event was well attended and even had representatives from SANSA in attendance. Presentations on other CubeSats included Denel Dynamics’ DynaCube, FUNcube-1 and SA AMSAT’s own KLETSkous project.

This paper gives a brief introduction to the F’SATI programme, the constructed CubeSat and mission. An outline of the milestones reached thus far with the Tshepiso nano-satellite are given, the outstanding activities that must still be completed and challenges faced. Some of the images captured by the satellite are also presented. Read TshepisoSAT, six months on orbit.
http://www.cput.ac.za/blogs/fsati/files/2014/05/Paper-SA-AMSAT-Space-Symposium-Pretoria-2014.pdf

CPUT F’SATI News http://www.cput.ac.za/blogs/fsati/blog/

Southern African Amateur Radio Satellite Association (SA AMSAT) http://www.amsatsa.org.za/

2014 FUNcube missions – May Update

UKube-1 ready for launch

UKube-1 ready for launch

The FUNcube team have received confirmation that UKube-1, which is hosting the FUNcube-2 payload, is now scheduled for a Soyuz-2-1b Fregat-M launch from Baikonur in Kazakhstan on Saturday, June 28 with the following day as a back-up.  The launch time has been quoted as 15:58:28 UT with separation some 9253 seconds later.

The team still understand that, immediately after deployment and activation, UKube-1 will commence transmitting a CW beacon and that this will be later followed by an AX25, 1200 bps BPSK beacon. Both beacons will be on 145.840 MHz. The FUNcube-2 payload, with its telemetry downlink for educational outreach, is expected to be tested later.

FUNcube-3 is the transponder only payload on the QB50 precursor CubeSat “QB50P1″. This mission is now scheduled to launch on June 19 on a Dnepr launch vehicle from Dombarovsky near Yasny. The launch time has been quoted as 19:11:11 UT but this has not yet been confirmed.  The initial beacon signals, from the main transceiver, are also expected to be AX.25, 1200 bps BPSK packets on 145.815 MHz.

Again more information will be provided as soon as it becomes available!

QB50p1 and QB50p2 - Image Credit ISIS

QB50p1 and QB50p2 – Image Credit ISIS

UKube-1 communications subsystem:
• 145.840 MHz Telemetry, CW, 1k2 BPSK
• 2401.0 MHz S Band Downlink
• 437.425-437.525 MHz UKSEDS myPocketQub Downlink
• 145.915 MHz FUNcube beacon
• FUNcube 400 mW inverting SSB/CW transponder
– 435.080-435.060 MHz Uplink LSB
– 145.930-145.950 MHz Downlink USB

QB50p1 communications subsystem:
• 145.815 MHz 1200 bps BPSK telemetry
• FUNcube inverting 400 mW SSB/CW transponder
– 435.035-435.065 MHz Uplink LSB
– 145.935-145.965 MHz Downlink USB

FUNcube website http://www.funcube.org.uk/

FUNcube Yahoo Group https://amsat-uk.org/funcube/yahoo-group/

FUNcube Forum http://forum.funcube.org.uk/