Inflatable Antenna Could Give CubeSats Greater Reach

CubeSat equipped with an inflated antenna, in a NASA radiation chamber - Image credit Alessandra Babuscia

CubeSat equipped with an inflated antenna, in a NASA radiation chamber – Image credit Alessandra Babuscia

MIT report researchers led by Alessandra Babuscia have developed a new design of antenna for small satellites known as CubeSats.

Professor Sara Seager KB1WTW - Image credit MIT

Professor Sara Seager KB1WTW – Image credit MIT

Due the their small size CubeSats have been restricted to small monopole or dipole antennas. Such low gain omni-directional antennas have restricted CubeSats to Low Earth Orbits (LEO) using lower data rates than would be possible with a large dish antenna.

The MIT team, led by Alessandra Babuscia, is part of the research group of radio amateur Professor Sara Seager KB1WTW and also includes graduate students Mary Knapp KB1WUA, Benjamin Corbin, and Mark Van de Loo from MIT, and Rebecca Jensen-Clem from the California Institute of Technology.

The new inflatable antenna developed by Alessandra Babuscia and her team may significantly increase the communication range of these small satellites, enabling them to travel much farther in the solar system: The team has built and tested an inflatable antenna that can fold into a compact space and inflate when in orbit.

It is claimed the distance that can be covered by a satellite with an inflatable antenna is seven times farther than that of existing CubeSat communications.

Alessandra Babuscia - Image Credit MIT

Alessandra Babuscia – Image Credit MIT

“With this antenna you could transmit from the moon, and even farther than that,” says Alessandra Babuscia, who led the research as a postdoc at MIT. “This antenna is one of the cheapest and most economical solutions to the problem of communications.”

‘Magic’ powder

An inflatable antenna is not a new idea. In fact, previous experiments in space have successfully tested such designs, though mostly for large satellites: To inflate these bulkier antennas, engineers install a system of pressure valves to fill them with air once in space — heavy, cumbersome equipment that would not fit within a CubeSat’s limited real estate.

Babuscia raises another concern: As small satellites are often launched as secondary payloads aboard rockets containing other scientific missions, a satellite loaded with pressure valves may backfire, with explosive consequences, jeopardizing everything on board. This is all the more reason, she says, to find a new inflation mechanism.

Mary Knapp KB1WUA - Image credit Interplanetary Small Satellite Conference

Mary Knapp KB1WUA – Image credit Interplanetary Small Satellite Conference

The team landed on a lighter, safer solution, based on sublimating powder, a chemical compound that transforms from a solid powder to a gas when exposed to low pressure.

“It’s almost like magic,” Babuscia explains. “Once you are in space, the difference in pressure triggers a chemical reaction that makes the powder sublimate from the solid state to the gas state, and that inflates the antenna.”

Testing an inflating idea

Babuscia and her colleagues built two prototype antennas, each a meter wide, out of Mylar; one resembled a cone and the other a cylinder when inflated. They determined an optimal folding configuration for each design, and packed each antenna into a 10-cubic-centimeter space within a CubeSat, along with a few grams of benzoic acid, a type of sublimating powder. The team tested each antenna’s inflation in a vacuum chamber at MIT, lowering the pressure to just above that experienced in space. In response, the powder converted to a gas, inflating both antennas to the desired shape.

Rebecca Jensen-Clem - Image credit Interplanetary Small Satellite Conference

Rebecca Jensen-Clem – Image credit Interplanetary Small Satellite Conference

The group also tested each antenna’s electromagnetic properties — an indication of how well an antenna can transmit data. In radiation simulations of both the conical and cylindrical designs, the researchers observed that the cylindrical antenna performed slightly better, transmitting data 10 times faster, and seven times farther, than existing CubeSat antennas.

An antenna made of thin Mylar, while potentially powerful, can be vulnerable to passing detritus in space. Micrometeroids, for example, can puncture a balloon, causing leaks and affecting an antenna’s performance. But Babuscia says the use of sublimating powder can circumvent the problems caused by micrometeroid impacts. She explains that a sublimating powder will only create as much gas as needed to fully inflate an antenna, leaving residual powder to sublimate later, to compensate for any later leaks or punctures.

MIT student with a CubeSat - Image credit MIT

MIT student with a CubeSat – Image credit MIT

The group tested this theory in a coarse simulation, modeling the inflatable antenna’s behavior with different frequency of impacts to assess how much of an antenna’s surface may be punctured and how much air may leak out without compromising its performance. The researchers found that with the right sublimating powder, the lifetime of a CubeSat’s inflatable antenna may be a few years, even if it is riddled with small holes.

Kar-Ming Cheung, an engineer specializing in space communications operations at NASA’s Jet Propulsion Laboratory (JPL), says the group’s design addresses today’s main limitations in CubeSat communications: size, weight and power.

“A directional antenna has been out of the question for CubeSats,” says Cheung, who was not involved in the research. “An inflatable antenna would enable orders of magnitude improvement in data return. This idea is very promising.”

Babuscia says future tests may involve creating tiny holes in a prototype and inflating it in a vacuum chamber to see how much powder would be required to keep the antenna inflated. She is now continuing to refine the antenna design at JPL.

Students build a 3U CubeSat - Image Credit NASA

Students build a 3U CubeSat – Image Credit NASA

“In the end, what’s going to make the success of CubeSat communications will be a lot of different ideas, and the ability of engineers to find the right solution for each mission,” Babuscia says. “So inflatable antennas could be for a spacecraft going by itself to an asteroid. For another problem, you’d need another solution. But all this research builds a set of options to allow these spacecraft, made directly by universities, to fly in deep space.”

Alessandra Babuscia is a Postdoctoral Research Associate at Massachusetts Institute of Technology (MIT). She has worked on several satellite projects including CASTOR, ExoplanetSat, Rexis and TerSat.

Source – MIT press release
http://www.mit.edu/newsoffice/2013/inflatable-antennae-could-give-cubesats-greater-reach-0906.html

Video: Loading the ISILaunch03 ISIPOD with ham radio CubeSats

ZACUBE-1, FUNcube-1 and HinCube in the pod

ZACUBE-1, FUNcube-1 and HinCube in the pod

Wouter Weggelaar PA3WEG has released a HD video showing the loading of three CubeSats, ZACUBE-1, FUNcube-1 and HiNcube, into their ISIPOD deployer in the ISIS clean room in Delft, The Netherlands.

This 3U ISIPOD is shared between three teams. First in is ZACUBE-1, second is FUNcube-1, and last in is HiNcube. The material was shot by Leon Steenkamp of the ZAcube-1 team, and kindly provided to me.

The stills are shot by Gerard Aalbers of the FUNcube-1 team, and Charl Jooste of the ZACUBE-1 team.

Watch Loading the ISILaunch03 ISIPOD with ZACUBE-1, FUNcube-1 and HiNcube

FUNcube-1 is in its Pod https://amsat-uk.org/2013/09/04/funcube-1-is-in-its-pod/

ISS Slow Scan TV Pictures

RS0ISS SSTV 20130904 1125Z - Image credit Pete Sipple M0PSX

RS0ISS SSTV 20130904 1125Z – Image credit Pete Sipple M0PSX

Pete Sipple M0PSX received these Slow Scan TV images from the International Space Station on September 4-5, 2013.

RS0ISS SSTV 20130905 1228Z - Image credit Pete Sipple M0PSX

RS0ISS SSTV 20130905 1228Z – Image credit Pete Sipple M0PSX

Other images received by Pete during the two-day MAI-75 SSTV experiment on the ISS can be seen at:

04 Sept 2013 http://www.essexham.co.uk/news/iss-sending-sstv-04-sept-13.html

05 Sept 2013 http://www.essexham.co.uk/news/images-from-iss-05-sept-2013.html

Space Station Slow Scan TV Active https://amsat-uk.org/2013/09/04/space-station-slow-scan-tv-active/

Advanced notification of SSTV activity from the ISS is usually posted at http://ariss-sstv.blogspot.nl/

RS0ISS SSTV 20130905 1035Z - Image credit Pete Sipple M0PSX

RS0ISS SSTV 20130905 1035Z – Image credit Pete Sipple M0PSX

A day in the life of a radio ham

A day in the life of a radio ham

SRM-sat features in this new amateur radio promotional video.

Watch A Day In The Life Of A HAM

FUNcube-1 is in its Pod

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

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

The AMSAT FUNcube team are delighted to be able to announce that the FUNcube-1 CubeSat has now completed all its final testing and been placed into its launch POD.

This work was completed during a three day programme at the premises of ISIS BV in Delft in the Netherlands and was finished, on time, late Wednesday afternoon on September 4, 2013.

FUNcube-1 is actually the middle 1U CubeSat of three sharing a 3U ISIPOD.  It is sharing the ISIPOD with ZACUBE-1 from South Africa  and HiNCube from Norway.

ZACUBE-1 prior to being shipped to the Netherlands

ZACUBE-1 prior to being shipped to the Netherlands

ZACube-1, in addition to carrying VHF and UHF communications equipment also has a 20 metre beacon which will operate on 14.099 MHz  This ISIPOD, with the spacecraft inside, will be transported to Russia, early next month, for launch and will eventually be attached directly to the launch vehicle.

FUNcube-1 carries a U/V linear transponder and the educational telemetry beacon using 1k2 BPSK for school outreach purposes.

The current launch information has lift off scheduled for late November.

Full initial orbit details and TLE’s, together with decoding software will be made available over the next few weeks.

ZACUBE-1 HF beacon antenna deployment unit - Image credit CPUT

ZACUBE-1 HF beacon antenna deployment unit – Image credit CPUT

FUNcube-1 communication subsystem:
• 300 mW Inverting linear transponder for SSB and CW
– Uplink      435.150 – 435.130 MHz
– Downlink  145.950 – 145.970 MHz
• 300 mW BPSK Telemetry  145.935 MHz

ZACUBE-1 https://amsat-uk.org/2012/08/25/14099-khz-cput-cubesat-to-launch-end-of-november/

HiNCube http://www.hincube.com/

A recent presentation about the FUNcube project by Graham Shirville G3VZV and Wouter Weggelaar PA3WEG can be viewed online at http://www.batc.tv/streams/amsat1311 or downloaded from http://www.batc.tv/vod/Funcube1.flv

AMSAT-UK FUNcube Mission Patch Rev4 20100609

AMSAT-UK FUNcube Mission Patch

A PDF of the slides from that presentation is here FUNcube_Colloquium2013a

FUNcube information sheets:
•  FUNcube_Project Information_aug2013
•  FUNcube_Educational_Outreach aug2013

FUNcube-1 https://amsat-uk.org/funcube/funcube-cubesat/

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

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

Some of the other satellites that may be on the same Dnepr launch vehicle are listed at https://amsat-uk.org/2013/08/22/dnepr-cubesat-launch/

AMSAT-UK on Facebook https://www.facebook.com/pages/AMSAT-UK/208113275898396
AMSAT-UK on Twitter https://twitter.com/AmsatUK

Join AMSAT-UK http://shop.amsat.org.uk/shop/category_9/Join-Amsat-UK.html

Final gluing of FUNcube-1 bolt by Wouter Weggelaar PA3WEG – Image credit Gerard Aalbers

Final gluing of FUNcube-1 bolt by Wouter Weggelaar PA3WEG – Image credit Gerard Aalbers

Radio hams to say “HI” to Juno on 10m

This computer-generated image depicts NASA's Juno spacecraft firing its Leros-1b main engine - credit NASA

This computer-generated image depicts NASA’s Juno spacecraft firing its Leros-1b main engine – Image credit NASA

NASA’s Juno mission is inviting amateur radio operators around the world to transmit a coordinated message on the 28 MHz band to the Juno spacecraft.

NASA’s Juno spacecraft will fly past Earth on October 9, 2013 to receive a gravity assist from our planet, putting it on course for Jupiter.

To celebrate this event, the Juno mission is inviting amateur radio operators around the world to say “HI” to Juno in a coordinated Morse Code message. Juno’s radio and plasma wave experiment, called Waves, should be able to detect the message if enough people participate.

Juno will have a better chance of detecting the signal from many operators if the signal is spread out across the spectrum. The Juno Waves instrument is a broadband receiver, and the detector being used for this event has a band width of 1 MHz. It is better for detection of the signal to have a broadband signal coming in.

For this experiment, the Juno team would like to ask those participating to spread out in frequency across the 10 meter band. They have supplied a table of suggested frequencies between 28 and 29 MHz, based on the last letter of your call. When the HFR receiver is tuned to 28MHz, the center frequency is 28.5 MHz. A 50 kHz high pass filter limits low frequencies hitting the detector, so the frequency table excludes 28.5 MHz ±50 kHz. The natural signals the team expect to measure at Jupiter will consist of a large number of discrete tones, so spreading the signals out in this manner is a good approximation to the signals Juno is expected to detect. But at Jupiter, they don’t expect to be able to decode CW in the telemetry!

The 28 MHz band was chosen for this experiment for several reasons. The Waves instrument is sensitive to radio signals in all amateur bands below 40 MHz, but experience with the University of Iowa instruments on the Galileo and Cassini earth flybys shows significant shielding by the ionosphere at lower frequencies. As sad as it sounds, the team hope for lousy band conditions on October 9, so an appreciable fraction of the radiated energy escapes the ionosphere into space, and is not refracted back down to the ground somewhere else on the planet.

Juno’s antenna consists of a pair of tapered 2.8 meter long titanium tubes, deployed from the bottom deck of the spacecraft under the +X solar array and magnetometer boom. A high impedance radiation resistant preamp sits at the base of the antenna and buffers the signals from 50 Hz to 45 MHz. The elements are deployed with an opening angle of about 120 degrees. Ten meters is above the resonant frequency of the antenna and NEC analysis indicates a lobe generally along the spin axis of the spacecraft. This will be good for detection on the inbound part of closest approach to Earth.

The Waves instrument uses four receivers to cover the frequency range of 50 Hz to 41 MHz. Signals up to 3 MHz are bandpass filtered, sampled by A/D converters and FFT processed into spectra using a custom FFT processor developed by The University of Iowa under a grant from the Iowa Space Grant Consortium.

The Juno team point out that All transmissions must follow local and national regulations.

Please join in, and help spread the word to fellow amateur radio enthusiasts!

NASA – Say “HI” to Juno! http://www.jpl.nasa.gov/hijuno/
See How do I participate ? for the frequency list.