Launch of EASAT-2 and HADES satellites

EASAT-2 and HADESThe EASAT-2 and HADES satellites, each carrying an FM transponder and digipeater, are expected to launch on January 13 at 15:25 GMT on the SpaceX Falcon-9 Transporter-3 mission.

A translation of a post by Spain’s URE reads:

The Scottish space broker Alba Orbital has confirmed the correct integration of the EASAT-2 and Hades satellites in the Falcon-9vehicle, using the company’s AlbaPOD ejector. It is confirmed, except for exceptional circumstances, the launch for this Thursday, January 13, initially at 15.25 UTC (16.25 Spanish peninsular time). Both satellites should have been launched a year ago, but the problems of the Momentusintegrator, on whose Vigoride vehicle albaPod ejectors of Alba Orbital were to be integrated with the American administration, caused this delay. Momentus was replaced by Exolaunch for the flight.

Both satellites offer FM voice communications and data relay in FSK or AFSK up to 2400 bps,such as AX.25 or APRS frames. They also broadcast voice beacons on FM with the callsigns AM5SAT and AM6SAT,as well as CW.

The EASAT-2satellite, designed and built jointly by AMSAT-EA and students of the European University of the Degrees in Aerospace Engineering in Aircraft and in Telecommunication Systems Engineering,with contributions from ICAI in the communications part, incorporates as experimental cargo basaltic material from Lanzarote,similar to lunar basalts, provided by the research group on meteorites and planetary geosciences of the CSIC at the Institute of Geosciences, IGEO (CSIC-UCM) and that could be used as a building material on the Moon. This project was promoted and has the collaboration of the ETSICCP (UPM).

The UNESCO world geopark of Lanzarote and Chinijo archipelago has been used for various investigations as an analogue of the Moon and Mars, including also the instruction of ESA astronauts. The selected basaltic material meets the requirements to be used as a simulant of the basalt existing on the Moon. The purpose of the experiment is to determine its evolution in space based on periodic measurements of some of its properties. Although the experiment is limited and constitutes a first phase of this type of study, it is an important milestone as it is the first of its kind introduced on such a small satellite.

As for Hades,its payload consists of a miniature camera module that sends the captured images as an audio signal in SSTVmode. The SSTV formats it uses are compatible with Robot36, Robot72, MP73 and MP115.

The design is based on the one used in the successful mission of the PSAT2satellite, an amateur radio satellite of the United States Naval Academy and brno University of Technology. This chamber has been operational since June 25, 2019: (http://www.aprs.org/psat2.html).

The camera chip is the Omnivision OV2640, which provides a resolution of up to 2M pixels and compressed output in JPEG. Resolution is limited by the CPU’s internal memory (MCU) that controls the camera to 320×240 (typical) or 640×480 maximum. The MCU selected for the control is the STM32F446RET6, which has the smallest possible footprint with connection to DCMI peripheral, necessary for connection with the camera.

Images can be stored on a 2 MB serial flash memory. The complete SSTV encoder has managed to be implemented in a 4-layer PCB with dimensions of only 38x38mm.

The MCU can be fully controlled from ground stations. The firmware allows the sending of images of the camera live,of imágenes previously saved in the flash memory or of images encoded in ROM. It also provides advance programming of image acquisition and PSK telemetry with the current status (event counters, temperature, voltage, light conditions, etc.) and a brief summary.

The described module has been developed and manufactured at the Department of Radioelectronics of the Brno University of Technology in the Czech Republic. Both hardware and firmware designs with the source codes will be available on Github under the MIT license (https://github.com/alpov/SatCam).

Initially only the EASAT-2 repeater is active. Hades’ will be activated by telecommand a few days after launch.

The frequencies coordinated with IARU for both satellites are as follows:

EASAT-2
  • 145.875 MHz uplink, Modes: VOICE FM (without undertone) and FSK 50 bps, AFSK, AX.25, APRS 1200 / 2400 bps
  • 436.666 MHz downlink, Modes: FM voice, CW, FSK 50 bps, FM voice beacon with AM5SAT callsign

HADES

  • 145.925 MHz uplink, Modes: VOICE FM (without undertone) and FSK 50 bps, AFSK, AX.25, APRS 1200 / 2400 bps
  • 436.888 MHz downlink, Modes: FM voice, CW FSK 50 bps, SSTV Robot 36, FM voice beacon with AM6SAT callsign

The description of the transmissions can be found in the following document:

EspañolEnglish:

AMSAT-EA appreciates the reception of telemetry, voice beacons and SSTV images. A paper QSL is sent to those who send their transmissions. It can be done through the following link: http://data.amsat-ea.org

Get The Details…

m5aka

AMSAT-UK

Powered by WPeMatico

First ever Svalbard QO-100 DXpedition JW100QO

Map of Svalbard showing the QO-100 station location

Map of Svalbard showing the QO-100 station location

A DXpedition to Svalbard (78° North) is planned for April 19-26 with the callsign JW0X. In addition to the five HF stations (FT8/FT4/RTTY/SSB/CW) the team will activate the first QO-100 satellite DX Station callsign JW100QO April 22-24.

Making the first ever QO-100 calls from Svalbard is the biggest challenge of this DXpedition. ON4CKM Cedric, ON4DCU Patrick and ON5UR Max will make a rugged snowmobile ride of almost 100 km in temperatures of -20° – 25° Celsius to reach their goal. Kapp Linné is the only place in the area that allows a view of the QO-100 satellite at only 3° above the horizon. Svalbard also lies on the edge of the satellite area (footprint), which makes the challenge even greater. We want to give as many radio amateurs as possible the opportunity to work this first QO-100 DXpedition. For this unique challenge we also have a special callsign JW100QO.

Further info at:

Svalbard QO-100 JW100QO April 22-24
https://www.dx-adventure.com/en/qo-100-our-goal/

Svalbard JW0X April 19-26
https://www.dx-adventure.com/en/svalbard-dx-pedition/

QO-100 geostationary amateur satellite transponder provides coverage from Brazil to Thailand, see
https://amsat-uk.org/satellites/geo/eshail-2/

Get The Details…

m5aka

AMSAT-UK

Powered by WPeMatico

FUNcube – Welcome to 2022

FUNcube-1 - Battery Voltage - Whole Orbit Data

FUNcube-1 – Battery Voltage – Whole Orbit Data

There are presently three FUNcube based missions in orbit – currently all of them have active, linear U/V transponders. The current status of each of these can always be checked on the useful AMSAT-NA status page https://www.amsat.org/status/ and an update on each of them is provided below. Please have FUN using them!

AO73 – FUNcube1. As previously reported AO73 appears to be experiencing some power issues after 8+years in orbit.

The battery is not charging to the same voltage as it did up to early November last year. The spacecraft has experienced many months of continuous sunlight over the past couple of years and this has resulted in high (around +30C) onboard temperatures. This environment may have “cooked” the cells although presently we do not see any direct evidence of this.

We can see that the stable bus voltage indicated at the end of charge is now much lower and depends on the current being taken by the on-board systems. The solar panel currents appear to be similar to those recorded soon after launch. The current best theory is that we are seeing the effect of some increased resistance in the supply circuit between the eps charging circuit and the battery. Although we do not have access to a fully detailed circuit diagram of the EPS we believe that there is an “ideal diode” in this line to prevent discharge of the battery back through the EPS circuitry. We understand that this is actually a MOSFET device and the suspicion is that this may now be showing signs of radiation damage.

So an operational mode has been selected that can be hopefully sustained for some time. From today AO73 is in continuous transponder mode and is available for use 24/7. Low power telemetry is also being transmitted and reports of the data are very welcome via the FUNcube Data Warehouse. Please remember that the uplink frequency varies with on board temperatures. A lower temperature means a higher frequency!

EO88 – Nayif-1. EO88 continues to perform nominally and is switching between high power telemetry for educational outreach when in sunlight and to its U/V transponder mode when in eclipse. It will soon celebrate its 5th birthday in space after launch on 15th February 2017.

JO97 – JY1Sat. JO97 suddenly stopped transmitting telemetry data on May 1st last year. The cause of this anomaly is unknown but fortunately the U/V transponder continues to operate continuously.

Battery voltage and incoming solar current over time - daily average

Battery voltage and incoming solar current over time – daily average

Get The Details…

m5aka

AMSAT-UK

Powered by WPeMatico

XW-3 (CAS-9) Satellite Launch December 26

XW-3 (CAS-9) satellite

The CAMSAT XW-3 (CAS-9) satellite carrying a 145/435 linear transponder has been installed on the CZ-4C Y39 launch vehicle at the Taiyuan Satellite Launch Center. The launch is scheduled for 03:11:31 GMT on December 26.

XW-3(CAS-9) satellite will be piggybacked on the rocket with primary payload ZY-1(02E) satellite. The satellite orbit is a circular sun-synchronous orbit with an altitude of 770.1 kilometers and an inclination of 98.58 degrees, the running cycle is 100.14 minutes.

The functions of XW-3(CAS-9) satellite include UHF CW telemetry beacon, GMSK telemetry data transmission, V/U mode linear transponder, a visible light band space camera and an experimental thermoelectric generator for high school students.

Deployment from the launcher will take place at  at 98.858° east longitude and 28.413° north latitude at 03:35:58 GMT, location close to Western Australia. Radio amateurs should receive CW beacon and GMSK telemetry signals approximately 38 seconds after the satellite is separated from the launch vehicle, and then the linear transponder will be put into use after approximately 49 seconds.

Download the XW-3(CAS-9) Amateur Radio Satellite User’s Manual V1.0

Download the XW-3 (CAS-9) Amateur Radio Satellite Launch Time Sequence

Download the XW-3 (CAS-9) Two-Line Orbital Element file

Get The Details…

m5aka

AMSAT-UK

Powered by WPeMatico

CAS-9 / XW3 to launch December 25

XW-3 (CAS-9) satellite

The CAMSAT XW-3 (CAS-9) satellite carrying a 145/435 linear transponder has been installed on the CZ-4C Y39 launch vehicle at the Taiyuan Satellite Launch Center, launch is expected on December 25.

XW-3(CAS-9) satellite will be piggybacked on the rocket with primary payload ZY-1(02E) satellite. The satellite orbit is a circular sun-synchronous orbit with an altitude of 770.1 kilometers and an inclination of 98.58 degrees, the running cycle is 100.14 minutes.

The functions of XW-3(CAS-9) satellite include UHF CW telemetry beacon, GMSK telemetry data transmission, V/U mode linear transponder, a visible light band space camera and an experimental thermoelectric generator for high school students.

Download the XW-3(CAS-9) Amateur Radio Satellite User’s Manual V1.0

Get The Details…

m5aka

AMSAT-UK

Powered by WPeMatico