I’m sorry to report that despite coordinated efforts between Japanese and European teams we have not been able to receive any signal from UNITEC-1 over Europe. Japanese ground stations were able to receive both the orbit determination downlink and the major/minor data downlink during the first pass after launch; however, the signal has been lost during the first mission day sometime between LOS over Japan and AOS over Europe.
The launch of H-IIA F17 carrying AKATSUKI, IKAROS, UNITEC-1 and three cubesats was successful! So was the separation of UNITEC-1 which was confirmed at 22:48 UTC (Epoch time 22:46:20 UTC).
We meet tomorrow afternoon at OZ7SAT for the first communication window predicted to begin around 17:21 UTC. At that time UNITEC-1 will already be at lunar distance! Until then, good luck to the Japanese ground stations with acquiring the first signals.
Yesterday was day 2 where we were repairing the broken Azimuth rotator and making a small 90cm dish ready to track UNITEC-1 on 5.84 GHz. Actually, we already fixed the rotator on Monday but we ended up mounting it 180° off and we decided to fix it properly instead of just correcting it in software.
Fixing the orientation of the Azimuth rotoator was very quick – it took only 17 minutes to get up to the mast, lift the antenna construction, change the orientation of the rotator and fasten the nuts and bolts again. We had the practice from yesterday.
Next item on the agenda was to make a small helix with two turns to feed the 90cm dish so that we can use this smaller dish for tracking UNITEC-1 in the beginning of the interplanetary cruise. We found some online helical antenna calculator to generate the design but that was more than 1 GHz off and it took a lot of tweaking and tuning to get it close to 5.8 GHz. Here are the results, photos and videos.
As you probably already know the UNITEC-1 launch got scrubbed today (17th May). Fortunately, there is a launch window every day for the next few weeks.
During the last few days I learned that tracking UNITEC-1 will be very difficult because the available trajectory data can be very uncertain. Therefore, we decided to use a smaller antenna with wider beam width in the first few days after launch. One option was to mount the IKEA dish to piggyback the 7m dish, another option was to use a 90cm dish which is currently equipped with a 2.4 GHz feed. We decided to go for the second option.
AMSAT OZ staff are preparing the 7 meter dish for tracking the UNITEC-1 interplanetary spacecraft.
Below you will find the link budget summary calculated for a few distances during the interplanetary cruise of UNITEC-1. The link budget calculator sheet containing all the details is available here.
|TX Power||4.8 W / 6.8 dBW / 36.8 dBm|
|TX Ant Gain||5 dBi|
|Free Space Loss||194 dB||214 dB||234 dB||251 dB||254 dB|
|Atm. losses||2 dB|
|Signal at RX ant||-184 dBW||-204 dBW||-224 dBW||-242 dBW||-244 dBW|
|Pointing loss||0.4 dB|
|Receiver G/T||23 dB/K|
|S/N0||67 dBHz||47 dBHz||27 dBHz||10 dBHz||7 dBHz|
|SNR @ 500 Hz BW||40 dB||20 dB||0 dB||-17 dB||-20 dB|
|SNR @ 100 Hz BW||47 dB||27 dB||7 dB||-10 dB||-13 dB|
- Attenuation due to rain, ionosphere and atmospheric gasses set to 2 dB
- TX power is 4.8 watts/antenna.
- TX antenna is microstrip patch, linear, assuming 5 dBi gain.
- Our beam width is 0.5° and I assumed a pointing error no greater than 0.1° (very optimistic) giving a 0.4 dB pointing loss.
TBDs and TBCs
- Measure the receiver noise floor, i.e. local interference contribution to sky temperature (important)
- Re-assess sky noise taking expected solar noise, etc. into account
- An optimistic estimate suggests that we should be able to receive UNITEC-1 up to 10-15 million km distance.
- There is plenty of margin in the beginning and we can use a low gain antenna for initial acquisition. The IKEA dish has ~25 dBi gain and it could be used up to 1 million km where after the trajectory is hopefully well known.
With only a few days left until the launch of UNITEC-1 (May 17) to Venus, we are getting ready to track it and I am trying to catch up on the documentation part – this time a brief description of the receiver hardware.
Recall the system architecture where the 5.84 GHz RF signal is converted to 640 MHz using the KU LNC 5659 C PRO low noise down converter, and…
This article gives a high level walkthrough of the receiver used to convert the 640 MHz IF to digital baseband, i.e. the blue box called USRP in the above diagram.
I have been playing with GNU Radio and GRC (GNU Radio Companion) over the weekend and I ended up implementing a very simple CW receiver. This will be very handy on Tuesday when we will be testing the 5.8 GHz UNITEC-1 setup for the first time using the OZ7IGY beacon on 5.76093 GHz. Here is a quick video demo of the receiver where I use my Yaesu FT-817ND to transmit a test signal.
Today I have been looking at the options for bias tees that we can use for the UNITEC-1 receiver. A bias tee (aka. Bias -T) is a simple device that can inject DC voltage into a coax cable. It is often used to provide supply voltage to devices that are mounted on the antenna without the need for dedicated DC cables. In our case, the low noise converter (LNC) will be mounted on the antenna and the “cable length” between antenna and control room is 40 meters, so it matters a lot that we can use the already existing RF coax cable to also supply the DC voltage. Actually, the KU LNC 5659 C PRO that we will use can only be supplied via the coax.
We have two Bias-T on stock: The KU BT 271 N from Kuhne that was originally acquired for the S-band ground station and something called MSTTR001 from Snec – don’t have much info about this one besides that it should be good up some-GHz and 100 mA current.
As you can see, the KU BT 271 N has two N-connectors while the Snec has two SMA connectors but is mounted on this adapter thing so that the antenna end has an N-connector. The USRP + WBX or TVRX receiver has SMA connectors and the coax cable has N-connector, thus it seems that the Snec would be best suited. Unfortunately, the LNC requires 180 mA so we’ll stick to the KU BT 271 N, which can be used up to 1 A.
- Structural Design of UNITEC-1 (944k PDF)
- UNITEC-1 and Onboard Computer Survival Competition in Interplanetary Environment (867k PDF)
- Preliminary Thermal Design of UNITEC-1 (1.0M PDF)
They all appear to be from the same conference held last year.
I also found two videos on YouTube, one showing a 20 second flight sequence, and one longer that appears to give a presentation of UNITEC-1; however, it is in Japanese so I have no idea what they say 🙂
If you find something else interesting about UNITEC-1, technical papers, videos or something else, leave a comment!
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