Received STRaND-1 9k6 signals

STRaND-1

After todays succesfull launch with a PSLV-C20 from Satish Dhawan Space Center (Sriharikota, India) the first signals are recieved from STRaND-1, this 3U nanosat that is build at the Surrey Space Centre (University of Surrey) using a Google Nexus-I as board computer. Here is a picture that I made from my reception this evening 25-feb-2012 19:00 UTC using a FUNcube Dongle Pro+, SDR# and a Maspro 435HS20.

STRaND-1 Reception 23-02-2013

The next couple of days I’ll try to decode the IQ data that was recorded during this pass. Lets see if we can find the 9600 baud data within this IQ stream. I have updated the STRaND-1 page with information to decode the telemetry using AGW Packet Engine and AGW KissOnline.

ISS Shadow Space plasma experiment

Space plasma experiment “Shadow” onboard International Space Station (ISS) with participation of radio amateurs.

Motivation and background

Many space professionals are looking forward to further space exploration using electric thrusters (ET). Unlike ordinary chemical propulsion systems, ET demonstrate much more higher exhaust velocity, since the propellant is accelerated for propulsion by electric power being supplied from an onboard source. The thrust produced by ET is very small – not more then a few grams so that ET cannot burst a rocket from the Earth surface. ET can tick only on board any orbiting satellite or spaceship.

The high exhaust velocity distinguished by ET offers noticeable propellant saving for given maneuver in space as compared to chemical propulsion so that mass reduction of a communication satellite for instance may be up to a few hundreds kilos. As a result this more lightweight satellite could be lifted in orbit by less heavy launch vehicle saving millions of dollars.

Money is not the only benefit

However money saving is not the only profit. A less heavy rocket is less hazardous for environment. ET themselves are ecologically pure using as non-detrimental propellants as noble gases, hydrogen, ammonia.

The benefit of electric propulsion will be more fully realized when significant cargo traffic arises in space providing deployment of large space structures, colonization of the Moon and planet exploration. That is why ET are included in such ambitious projects currently under development as Electric Orbit Transfer Vehicle, Lunar Ferry and some unmanned mission to planet. Over these projects the flight use of ET would save hundreds millions of dollars with better ecology.

Currently we are present at the beginning of the “gold century” of electric propulsion. To make it reality the electric propulsion community in many countries is going on with research and development of ET of different types either for secondary on-orbit application or for primary propulsion of multikilowatt level.

However what is a place of radio amateurs in the matter?

However what is a place of radio amateurs in the matter – an impatient reader could ask. Do not be in a hurry, dear reader, do not put reading this article off and you in a few minutes realize that the VHF-community could play its role in ET implementation if wants.

Integration of ET with onboard equipment poses a certain set of problems to be solved such as electromagnetic compatibility of ET. Particularly the matter is that highly ionized exhaust plumes of ET may scatter RF-signals producing large “dead” zone for communications.

This plasma screening effect should be thoroughly studied before electric thrusters become standard onboard equipment. The investigation will help designers of future electrically propelled spacecrafts to minimize the hazard of communication disruption by ET plasma plumes.

A little piece of history

In 1987 specialists of Central Research Institute of Machine Building (TSNIIMASH) conducted a series of space plasma experiments in order to evaluate the shape of mentioned above “dead” zone using KOSMOS satellites with onboard arcjet plasma source.

The well known method of radio sounding was used for plasma monitoring. The telemetric and command signals emitted by onboard antennas played a role of sounding signals. Passed through plasma these signals were simultaneously received by a number of on-ground measuring sites. The shadow effect was clearly observed however the precise data on the shadow boundary shape and its dynamics could not be obtained in the experiments of 1987 since the receiving network was too rarefied. Deployment of properly dense special receiving network is extremely expensive and consequently unrealistic.

We need receiving mosaics!

Possible solution is to use available worldwide spread network of amateur VHF receivers. This idea was put in the base of an proposal to perform a new plasma space experiment on the International Space Station (ISS) almost in the same layout as in 1987.

Methodologically SpEx “Shadow” is oriented to using of amateur packet radio and Internet technology and resources.

SpEx “Shadow” objectives and lay out

The objectives of the work is observation and evaluation of refraction/scattering effects in artificial plasmas using method of RF sounding in space experiments under different geophysical conditions.

ISS Plasma Shadow Area

SpEx “Shadow” lay out is shown in Fig.1. In the chosen region the onboard arcjet source injects a plasma plume in space and the onboard radio beacon transmits VHF sounding signals in the form of the Universal Time marks. Passed through the plasma these signals are being instantly received by an on-ground measuring VHF network. Due to refraction/scattering of the sounding signals in the exhaust plume, the shadow region would arise adjacent to the satellite. When the shadow boundary running after the satellite along the Earth surface reaches any on-ground receiving site the signal cut-off is to be registered. The task of every individual participant is to register moments of signal cut-off and following signal restore using the Universal Time marks and to address this information along with data on its geographical position to the Information Storing Center. Every operation sequence would take 6-8 min. while the satellite is passing between two opposite points of the local radio horizon. It is interesting to perform the experiment in different geophysical conditions.

Packet radio and Internet

The amateur packet radio technology in the SpEx “Shadow” as proposed by astronaut Alexander Kalery, offers the possibility to use Internet transport resources either for net-work notification or for data collection. Principally the available receiving network may be provided with Universal Time Marks if the onboard radio beacon merely transmits packets of minimal duration in format of AX25 Protocol.

This promises to perform large-scale monitoring of an artificial plasma nonhomogeneity using the mosaics of on-ground receiving sites.

The same technology can be also applied in space experiment on sounding of not artificially injected plasma, but of the natural ionospheric plasma in HF frequency band (14 MHz). It is expected, that due to dispersion of sounding radiation in ionospheric plasma, an “irradiated” spot should appear on the Earth surface, and determination of boundaries of this “irradiated” spot is the purpose of space experiment (legend “Spot”), which can be carried out not necessarily on the ISS.

Expected results

The scientific results the SpEx “Shadow” will help designers of future electrically propelled spacecrafts to minimize the hazard of communication disruption by ET plasma plumes.

Except the scientific issues, realization of the space experiment “Shadow” will give an unique experience in involving of intellectual and technical potential of International radio amateur community as well as Internet technology and resources for monitoring of the near-Earth space and to evaluate capability to use this potential in perspective scientific projects.

Actually the space experiment “Shadow” is an interesting attempt to use Internet for principally new goal – not only for information spreading but also as an effective measuring tool in spatially large-scale scientific researches.

The space experiment “Shadow” may also bring an important social result attracting public attention to advanced technology, astronautics, amateur packet radio and Internet.

With really mass, voluntary and gratuitous participation of VHF-amateurs this project would become a humanitarian world wide action uniting many peoples of different countries with interesting and useful work for future enhancing the spirit of cooperation, mutual understanding and friendship.

How it will be if will be

As it was mentioned above the space experiment “Shadow” may be successfully performed under the condition that the number of participants will be great enough . The greater this number the more precise scientific result would be issued.

As claims for participation in the SpEx “Shadow” appear at the Information Storing Center in response to this initial invitation, we are going to select perspective “measuring fields” where the receiving network is dense enough and where the bulk of activity will be further concentrated.

The SpEx “Shadow” will be performed in two stages:

  • of “cold” (with no plasma injection) planned over February – June 2011 as a SpEx “Shadow-beacon” (beacon for shadow) and
  • of full scale “hot” (with plasma injection) experiments.

After successful fulfillment of the “cold” phase it will be possible to accept the justified solution on realization of a series of full scale “hot” experiments later.

What to do if You decide to participate

If you do not mind to take part in the experiment, do as follows:

  1. Visit www.tsniimash.ru, page SpEx “Shadow-beacon”, make registration and subscription for news;
  2. e-mail your decision to the Information Storing Center shadow@tsniimash.ru or vastra@mail.ru with short personnel data: name, call sign, QTH, available radio equipment, your wish on experiment run conditions (day or night time, week-end and so on);
  3. Look through the available results of observation;
  4. Permanently look through current news;
  5. Take part in experiment runs and e-mail your report (log-file) to the Information Storing Center;

Every participant of the space experiment “Shadow-beacon” will be awarded with special certificate.

[PE0SAT Thanks Oleg Alifanov for the Above information (Website)]

ESA – Fly Your Satellite

P-POD IntegrationESA invites European student teams who are building CubeSats with mainly educational objectives to propose their satellite for the new ‘Fly Your Satellite!’ programme.

‘Fly Your Satellite!’ is an exciting new initiative from the ESA Education and Knowledge Management Office. It is focused on CubeSat projects run by university students and builds on the successful ‘CubeSats for the Vega Maiden Flight’ pilot programme, which culminated in 2012 with the launch of seven university student-built CubeSats on board the Vega Maiden Flight. 

In the future, this new initiative is intended to cover the complete development process of a satellite from concept to launch. However, the 2013 edition will be dedicated to teams whose satellite is already at an advanced stage of development and able to complete the Flight Model assembly by June 2013. One, two or three-unit CubeSats are eligible.

The ‘Fly Your Satellite!’ programme envisages three consecutive activity phases, with intermediate reviews that the student teams will have to pass to be accepted into the next phase.

Phase 1: Build Your Satellite

During Phase 1 the CubeSat teams shall complete the integration and functional testing of their CubeSat’s Flight Model in ambient conditions. They shall submit related documentation and data packages to be compiled following ESA guidelines.

At the end of Phase 1, the CubeSats development status and their data package documentation will be reviewed by ESA specialists who will select the teams for Phase 2 (the environmental test campaign).

Phase 2: Test Your Satellite!

CubeSat Clean before integrationA CubeSat team cleaning their CubeSat before integration.

During Phase 2 the selected teams will be supported by ESA during the task of performing environmental tests on their satellites. These will include vibration and thermal-vacuum tests. For this activity, ESA will offer the use of a Thermal Vacuum chamber and a mechanical shaker.

The definition of the launcher and the mission’s environmental requirements are not yet expected to be known by the time of Phase 2. Therefore the environmental tests will be performed against an envelope of generic requirements that will be agreed between the ESA specialists and the CubeSat teams.

During this phase, in which the satellite performances will have to be assessed before and after the test campaign, the teams shall prepare and then submit the so-called Acceptance Data Packages. These shall be compiled following ESA guidelines and shall include the documentation of the test campaign.

At the end of Phase 2, the satellites’ documentation will be reviewed by ESA and the best CubeSat teams will be selected for a launch opportunity – their Ticket to Orbit!.

Phase 3: Ticket to Orbit!

Xatcobeo final assemblyThe ESA Education Office will facilitate the procurement of a launch opportunity that is still to be defined. Therefore, start-time and duration of Phase 3 will depend on the actual launch date.

The CubeSats selected for a Ticket to Orbit! will be launched if and only if the respective teams provide proof of the CubeSat frequency registration with the International Amateur Radio Union (IARU) and the International Telecommunication Union (ITU), and proof of the satellite’s registration on the United Nations (UNOOSA) Register of Objects Launched into Outer Space.

The selected CubeSats will be installed inside CubeSat orbital deployers, and, after a campaign of integrated tests (to be performed against the environmental requirements of the real mission), the flight hardware will be shipped to the launch site for the launch campaign.

Further details can be found at the ESA website via the this URL

[PE0SAT Thanks ESA and PA0DLO for the above information]

ISS Plasma Thrust Shadow-Beacon Experiment

It is understood that the ISS amateur radio SpEx Shadow-Beacon experiment is planned to take place February 1-3 and 8-10. The timetable is here.

ISS and Shuttle

The Central Research Institute of Machine Building (TSNIIMASH) in Russia is conducting a series of space plasma experiments in order to evaluate the shape of previously observed “dead” zone, or shadowing due to the firing of an onboard arcjet plasma source.

Radio Amateurs are invited to participate in the Space plasma experiment “Shadow” onboard the International Space Station (ISS).

Integration of Electric Thrust (ET) onboard a spacecraft poses a certain set of problems including electromagnetic compatibility of ET. One matter of interest is that highly ionized exhaust plumes of ET may scatter RF-signals producing large “dead” zone for communications.

This plasma screening effect should be thoroughly studied before electric thrusters become standard onboard equipment. The investigation will help designers of future electrically propelled spacecraft to minimize the hazard of communication disruption by ET plasma plumes.

The experiment will use the ISS Amateur Radio 145.825 MHz FM AX.25 1200 bps packet radio downlink.

The amateur packet radio technology in the SpEx “Shadow” as proposed by astronaut and radio amateur Alexander Kaleri, U8MIR, uses the AX25 packets transmitted by “Master Stations” and reported by receiving amateur radio ground stations to track the effect of the plasma shadow.

SpEx Shadow sample report http://www.terranimpact.com/site/space/sampl_report.doc The main web page for the SpEx project can be found at http://knts.tsniimash.ru/Shadow/en/Overview.aspx

An example of the SpEx packets received by Mike Rupprecht, DK3WN is at http://www.dk3wn.info/p/?p=23866

[PE0SAT Thanks Amsat-UK and M5AKA for the above information]

Fitsat-1 live Led experiment

FITSAT-1 LedsFitsat-1 (Niwaka) Led Experiment over Europe

On December 13 at 22:10 UTC (23:10 CEST) The Fitsat-1 LED experiment will be active over Europe. Let’s hope it’s a clear night, so we all can see the 200W LED display sending Morse code in the sky.

Fitsat-1 Led Experiment Orbit over Europe

Maybe it is possible to make a picture or a little video from the experiment when it passes your locator. Maybe it is possible that you send me a copy. Everybody have fun observing the Fitsat-1 Led experiment.


FITSAT-1 Successfully Flashes Morse Code from Space

A test of the FITSAT-1 LED optical beacon that took place on December 11 GMT over Japan was successful.
Fitsat-1 LED Beacon
(C) Tsuyoshi Watanabe Ebina City, Kanagawa Japan 1:24:23-1:24:25JST, 12 Dec 2012 Takahashi e160, Diameter short focus telescope 16cm (F=530mm, F3.3) Nikon D800E, ISO12800, 2 seconds exposure.

[PE0SAT Thanks Amsat UK and Tsuyoshi Watanabe for the above information]

FO-29 close approach

FO-29Space debris close to the FO-29

The United States Joint Space Operations Center (JSpOC) has identified a predicted conjunction between JAS 2 (SCC # 24278) and SCC # 10470.

Primary Object: JAS 2 (SCC # 24278)
Secondary Object: SCC # 10470
Time of Closest Approach: 23 NOV 2012 23:38 UTC

Overall miss distance: 984 meters
Radial (dU) miss distance: 174 meters
In-Track (dV) miss distance: 690 meters
Cross-track (dW) miss distance: -680 meters

Primary Radial Error (U): 14 meters
Primary In-track Error (V): 104 meters
Primary Cross-track Error (W): 16 meters

Secondary Radial Error (U): 25 meters
Secondary In-track Error (V): 350 meters
Secondary Cross-track Error (W): 11 meters

JSpOC Orbital Protection Team

Joint Space Operations Center
Vandenberg Air Force Base, California USA


Original post: FO-29 weblog (Google translation)