PhoneSat project

NASA Ames Research Center continues work on its PhoneSat project, which is demonstrating the ability to build very-low-cost satellites using Android smartphones as processors.

Ames has built two versions of the PhoneSat – PhoneSat 1, which costs about $3500, and PhoneSat 2, which costs just under $8,000. Both versions are based on HTC Nexus One smartphones. The first PhoneSats are scheduled to be launched aboard an Orbital Sciences Corporation Antares launch vehicle. The launch, funded under the Commercial Orbital Transportation Services (COTS) program, is scheduled for the third quarter of 2012. It will carry two PhoneSat 1 satellites and one PhoneSat 2. A second PhoneSat launch is expected to occur in 2013.

Videos of 9th Annual CubeSat Developers’ Workshop

The Spring CubeSat workshop held April 18-20 proved a great success and videos of the event are now available.

Spring Workshop Videos http://mediasite01.ceng.calpoly.edu/Mediasite/Catalog/pages/catalog.aspx?catalogId=64b6f338-8445-475b-9062-84c90d54ff45

Spring Workshop Schedule http://www.cubesat.org/images/2011_Spring_Workshop/2012_workshop_schedule1.pdf

Videos of 9th Annual CubeSat Developers' Workshop

The Spring CubeSat workshop held April 18-20 proved a great success and videos of the event are now available.

Spring Workshop Videos http://mediasite01.ceng.calpoly.edu/Mediasite/Catalog/pages/catalog.aspx?catalogId=64b6f338-8445-475b-9062-84c90d54ff45

Spring Workshop Schedule http://www.cubesat.org/images/2011_Spring_Workshop/2012_workshop_schedule1.pdf

Missions of KSAT2

 

1. Study on Forcast of Localied Downpour and TornadoIn-orbit experiments of an original observation method of atmospheric water vapor.
2. Take Earth Live Images from Space
Ku-band high-speed data transmission, one shot / a few seconds.
3. Basic Experiments for LEO Positioning Satellites
Frequency and phase synchronization between a ground-base system and a satellite.
4. Orbit Determination Experiments with Radio Interferometer
Essential item for nano-satellite orbiting at very low earth orbit.
5. Satellite Tracking Experiment at Very Low Earth Orbi Evaluation of Earth’s atmosphere to the satellite.
6. Verification of Pantograph-type Extending Boom in Space
The boom was originally designed and is fit for compact satellites.
7. Messages of Encouragement from Space to Japan. Hand-lettered messages and heart warming pictures, especially from children responsible for the future.

Communication

Dual uplink, Dual downlink and a beacon signal.

– Frequency and Transmissio Rate –
Frequency Band Moduration Method Transmission Rate Purpose
Uplink UHF Band F2D 1 kbps  Commands
S Band G2D 1 kbps  Command (Backup)
Downlink S Band G1D 200 ksps  HK Data
Ku Band G1D 1 Mbps or Carrier  Image and Beacon

  # Coding by viterbi algorithm is applied to S-band downlink data. 

Main body of the satellite has a shape of 10 cm Cube, and its mass will be 1.5 kg. An expanding boom for attitude control and two solar paddles are attached to the main body.

Student Nanosat VELOX-I

VELOX-I 640Over 150 students at the Nanyang Technological University in Singapore have worked on the innovative nanosat project VELOX-I.

Velox-I - N-Sat and P-SatVELOX-I consists of two satellites: a 3U nano-satellite N-Sat and a 1U pico-satellite P-Sat. N-Sat is developed to be a robust satellite bus for future missions, and P-Sat is an experimental design to carry a scientific payload. During the mission P-Sat will be released by N-Sat.

The VELOX-I mission includes demonstrating high-resolution vision subsystem, testing a MEMS-based attitude determination and control system, verifying intersatellite RF link, and performing a quantum physics experiment.

It is hoped it will launch in 2013, a downlink of 145.980 MHz has been coordinated.

This article ‘Over 150 students helped to build it’ by Tong Su Yee appeared in The New Paper
http://www.edvantage.com.sg/edvantage/news/schoolnews/699350/Over_150_students_helped_to_build_it.html

Students reach for stars with own satellite
http://www.eee.ntu.edu.sg/Documents/Students%20reach%20for%20stars%20with%20own%20satellite.pdf

Entangled Photon Systems for Small Satellites http://quantum.nasa.gov/materials/2012-01-21-A3-Ling.pdf

Nanyang Technological University VELOX-I http://www.sarc.eee.ntu.edu.sg/Project/Pages/VELOX.aspx 

The IARU Amateur Satellite Frequency Coordination Status http://www.amsat.org.uk/iaru/

16 Japanese Educational Satellites to be Launched

Kibo Robot Arm CubeSat Deployment

Kibo Robot Arm CubeSat Deployment

Sixteen educational satellites are under construction in Japan. The first should be launched in May 2012 followed by the others over the next two years.

Horyu-2 Structural Thermal Model

HORYU-2 Structural Thermal Model

The first to launch is the amateur radio satellite HORYU-2 built by students at the Kyushu Institute of Technology (KIT). The launch is on a Japanese H-IIA rocket planned for May 17 at 1639-1642 UT.

The mission aims to take pictures of the Earth using a small CMOS camera SCAMP (Surrey Camera Payload) developed by the University of Surrey, a sister university of KIT. SCAMP takes a 640×480 pixel picture in a JPEG format. From 700 km altitude, one pixel corresponds to 1.6 km.

HORYU-2 will be followed in July by the launch of the HTV3 to the International Space Station (ISS). This will deliver the JEM-Small Satellite Orbital Deployer (J-SSOD) along with the Japanese CubeSats WE-WISH, FITSAT-1 and RAIKO. These CubeSats should be deployed from the ISS in September using the Japanese Experiment Module (JEM) robot arm.

Takushi Tanaka JA6AVG and FITSAT

Takushi Tanaka JA6AVG and FITSAT

FITSAT-1, also known as NIWAKA, will use a neodymium magnet for attitude control. It has multiple downlinks, CW on 437.250 MHz, AX.25 on 437.445 MHz and a 4 watt high speed data transmitter on 5840 MHz capable of sending a 640 by 480 VGA JPEG image in 6 seconds.

In addition it carries high power LEDs that will be driven with 100W pulses to produce extremely bright flashes. These, it is hoped, will be observable by the unaided eye or with small binoculars. Both the 5840 MHz and optical downlinks have a high power consumption so it may be that they are only activated over Japan.

In December TSUBAME is planned to be launched on a H-IIA. It aims to have a CW beacon on 437.250 MHz and AX.25 1200/9600bps telemetry on 437.505 MHz.

The satellite blog run by Mineo Wakita JE9PEL is a good source of information on Japanese satellites, see http://tinyurl.com/JE9PEL-Satellite-Blog

The satellite blog of Nader Omer ST2NH contains a summary of Mineo’s information which is reproduced here:

Horyu-2
http://kitsat.ele.kyutech.ac.jp/what_horyu2_2.html
437.375MHz 1200bps FSK CW
——————————————————————————-

RAIKO
http://www.astro.mech.tohoku.ac.jp/RAIKO/
2U (10 cm by 10 cm by 20 cm)
——————————————————————————-

FITSAT-1
http://www.fit.ac.jp/~tanaka/fitsat.shtml
437.250MHz CW, 437.445MHz FM, 5840.00MHz High speed data
——————————————————————————

WE WISH
http://www.meisei.co.jp/news/2011/0617_622.html
IR pictures of the earth surface with 320×256 pixels
that will be downlinked in approx 110 secs using SSTV.
437.505MHz SSTV, Telemetry, CW

http://www.meisei.co.jp/english/news/2011/0617_636.html (English Version)

—————————————————————————–

STARS-II
http://stars1.eng.kagawa-u.ac.jp/
437.245MHz CW (mother), 437.255MHz CW (daughter)
437.405MHz FM (mother), 437.425MHz FM (daughter)
—————————————————————————-

TeikyoSat
http://sites.google.com/site/spacesystemteikyo/Home/teikyo-sat
—————————————————————————-

Komolebi
http://www.nano-sat.org/shinshu/files/2010shinshu/09_okamoto.pdf
—————————————————————————-

KSAT2
http://leo.sci.kagoshima-u.ac.jp/~n-lab/KSAT-HP/Ksat2.html
—————————————————————————-

INVADER
http://artsat.jp/
—————————————————————————-

OPUSAT
http://www.sssrc.aero.osakafu-u.ac.jp/OPUSAT_home.html
—————————————————————————-

ITF-1
http://yui.kz.tsukuba.ac.jp/
Mission 1 Establish human network by amateur satellite
Mission 2 Prove the ability of the micro engineered 1/20 wavelength small antenna
Mission 3 Prove the stable operation of FRAM based microcontroller and
other microcontroller in space environment
437.425 MHz
—————————————————————————-

RISING-2
http://www.astro.mech.tohoku.ac.jp/RISING-2/
—————————————————————————-

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

UNIFORM-1
http://www.wakayama-u.ac.jp/ifes/news/20120328.html
—————————————————————————-
SOCRATES
http://www.aes.co.jp/company/
—————————————————————————-

TSUBAME
http://lss.mes.titech.ac.jp/ssp/tsubame/
437.505MHz AX.25/SRLL, 9600bps GMSK, 1200bps AFSK
437.250MHz CW
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