Launch News Anticlimic 1st voyage of a superstar! Long March 6 test flight, September 19/20, 2015

Cosmic Penguin

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CZ-6_2big.jpg


In a few hours time, one of the largest milestones of recent Chinese spaceflight history (especially on the rocketry section) will occur - and we won't know anything about it had not been the fact that amateur radio operators are waiting for this one! :ninja:

The maiden flight of China's next generation rockets and 2 of the new rocket engines that will support the future of China's universal ambitions is less than 3 hours away. Yet unlike its larger sisters Long March 5 and 7, the Vega class Long March 6 was developed in almost complete secrecy and only one single photo of a completed launch vehicle has ever been leaked out!

Departing from every single previous Chinese design, the Long March 6 is the country's first clean sheet design rocket to fly, and the first one to fly from China with a kerosene/LOX powered engine. Both main stages of this Vega class launcher (more than 1 tonne to a 700 km SSO) are using completely new engines that will face their ultimate test in a few hours time, a moment that Chinese engineers have worked for the past 1.5 decades to reach.

Firstly, we have the YF-100 staged combustion kerolox engine, China's answer to an universal next generation engine that will literally boost their space dreams. For it will be used on all the first stages of the Long March 6/7 rockets, as well as the boosters on the Long March 5/7, lifting everything from small satellites in the "Vega class lift" requirements to lunar sample return missions and space station modules needing something in the Ariane 5 class!

This 1200 kN (270000 pounds of force) thrust engine (closest to the NK-33/AJ-26 in terms of thrust and specific impulse) was apparently developed using a Soviet RD-120 engine (used on the Zenit rocket's 2nd stage) sold to China in the late 1990s as a reference, but with 50% larger thrust. Of course the Chinese can't just copy it so it took more than 10 years to finally get this engine to the flight test phase. :hmm:

The 2nd stage engine is completely new too, though we don't know too much about it. The YF-115 engine is also a staged combustion kerolox engine an order of magnitude smaller than the first stage engine, providing about 175 kN (40000 pounds of force) during its flight. This engine will also be used for the 2nd stage of the Long March 7 rocket (4 engines on that stage) so we will probably also see it in action later. There is supposed to be a 3rd trim stage on this rocket too, although nothing is known about it.

This crucial first flight of one of the world's most used rockets in the future is about to happen today at 23:00 UTC at a top secret new pad at the Taiyuan Satellite Launch Center in northern China. The passengers on board are 20 small satellites from various Chinese institutions - at least 8 of them are amateur ham radio satellites that people worldwide will be able to track. Unfortunately we still don't know some of the passenger's identities at such a late stage! :facepalm:

I have absolutely no idea why the Chinese put this launch in complete secrecy :uhh: (there has been ZERO announcements from official channels for the past few months; compare with the Russians where they keep track of the development of the Angara and made one live broadcast attempt), but this one certainly needs more luck than many others.

:hailprobe:
 
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Soheil_Esy

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Part 1

Mission Briefing
Launch date: 2015-09-20/07:01:14.331 (GMT+8)
Launcher: CZ-6
Payload(Country): 20 nano satellites*(PRC)
Launch site(Country): Taiyuan(PRC)
Launch pad: New launch pad LC16 ( 1601 )
Status: Success
Orbit type and parameter: SSO 530 x 530km; inclination 97.47
Remark: maiden flight

*Complete payload list
1 哈工大紫丁香二号 Lilacsat2 11 kg
2 浙大皮星二号A ZDPS2A 0.2 kg
3 浙大皮星二号B ZDPS2B 0.2 kg
4 清华大学紫荆一号皮型卫星 ZJ-1 0.234 kg
5 清华大学紫荆二号皮型卫星 ZJ-2 0.173 kg
6 清华大学纳星二号 NS-2 20 kg
7 国防科大天拓三号 Luliang-1 20 kg
8 国防科大智能号手机卫星 NUDTPhone 1 kg
9 国防科大星辰号飞卫星1 XC 1 0.1 kg
10 国防科大星辰号飞卫星2 XC 2 0.1 kg
11 国防科大星辰号飞卫星3 XC 3 0.1 kg
12 国防科大星辰号飞卫星4 XC 4 0.1 kg
13 深圳东方红海特开拓一号 Kaituo-1A 130 kg
14 DCBB Kaituo-1B 3 kg
15 航天东方红希望二号A XW-2A 25 kg
16 航天东方红希望二号B XW-2B 10 kg
17 航天东方红希望二号C XW-2C 10 kg
18 航天东方红希望二号D XW-2D 10 kg
19 航天东方红希望二号E XW-2E 1.5 kg
20 航天东方红希望二号F XW-2F 1.5 kg
Note: speculative acronyms, mass discrepencies

Total mass about under 250 kg

Country Record number of satellites launched with a single rocket Launch date
China 3 satellites on Sept 20, 1981 (Now 20. After 34 years)
India 10 satellites on April 28, 2004
USA 29 satellites on Nov 19, 2013
Russia 32 satellites on Nov 21, 2013

2015/09/20

China successfully launched the first Long March 6 carrier rocket on Sunday morning, the first of a new generation of rocket families designed to boost the country’s space capabilities, including constructing a space station and future lunar missions.

The Long March 6 blasted off from the Taiyuan Satellite Launch Centre in the northern province of Shanxi at 0700 Beijing time (2300 UTC, September 19), sending a payload of 20 small satellites into Sun synchronous orbit.

The satellites, developed by a number of universities and space research institutes across China, include nine amateur radio satellites. The satellites separated from the rocket 15 minutes after blasting off from Taiyuan.

With Chinese authorities and media remaining quiet, online posts from those involved with amateur radio satellites offered the first indications that the launch was successful.

The liquid-fuelled Long March 6 was developed by the Shanghai Academy of Spaceflight Technology, and designed to be a more adaptable, reliable and responsive launch vehicle. Notably, it greatly increases China’s rapid response launch capabilities.

While the Long March 6 has only a modest lift capability of 1,080 kg, the launch was the crucial first full flight test of the new YF-100 engine, which is required to make China's ambitious space plans possible.

The YF-100 will power the Long March 5, China’s new heavy-lift launch vehicle which is roughly comparable in lift capability to the US Delta-IV Heavy. The Long March 5 is set to make its debut flight early next year.

A problem with the Long March 6 first stage engines would thus have been a serious blow to China’s space program and could have brought significant delays.

The first attempt at the launch, 24 hours earlier on Saturday morning, was reportedly scrubbed ten minutes before lift-off for technical reasons.

Space station and Moon mission plans

The Long March 5 is crucial to China’s future space ambitions, boosting lift capacity by around three times and will thus be relied upon to launch modules for the country’s upcoming space station, as well as a lunar sample return mission set for 2017.

Joan Johnson-Freese, Professor of National Security Affairs at the US Naval War College, expressed her personal view to gbtimes ahead of Sunday's launch that the Long March 5 that will signal a leap forward in Chinese capabilities.

“China’s three step human spaceflight program, Shenzhou, relies on the Long March 5 to lift its large space station to orbit, and in order to do a human lunar mission - anticipated as their “next step” - the Long March 5 is needed as well,” Johnson-Freese explains.

Professor Huang Jun at the Beijing University of Aeronautics and Astronautics told gbtimes that the new rockets mark a technological breakthrough for the country:

“This new generation of Chinese launch vehicle series uses universal modularized design which can be easily combined into new rocket variants for various missions. The reliability and launch preparation time are improved and the launching cost will be lowered.”

Huang also notes that the incendiary agents used for the new rockets are kerosene and liquid hydrogen, which are considered non-toxic, low or non-polluting when compared with the highly toxic unsymmetrical dimethyl hydrazine (UDMH) used in the currently used Long March 2, 3 and 4 series.

'Expanding capabilities'

The Long March 5, 6 and 7 rocket families are expected to provide increased reliability and adaptability, as well as lower launch costs and shorter preparation time. As the rockets mature over the next decade, they will replace their hydrazine-fuelled predecessors.

As well as developing new rockets, China has constructed a brand new launch base on the southern island province of Hainan.

The Wenchang Satellite Launch Centre, from which launches will take advantage of the Earth’s greater rotational speed at lower latitudes, took six years to construct and cost an estimated five billion yuan (US$800 million) and is another crucial component in China’s plans.

Wenchang has dedicated launch towers for the Long March 5 and the medium-lift Long March 7, both of which will be used for constructing and servicing the upcoming space station, and any interplanetary missions.

“What this means for the US and all space faring nations is another indicator that China is a long-term player in space with expanding capabilities. It cannot be denied or ignored, as the US has tended to do,” Johnson-Freese states.

http://gbtimes.com/china/china-launches-first-its-next-generation-rockets

CZ-6 launcher

2015-09-20

According to an article in the Journal of the Chinese army, CZ-6 is designed and produced by SAST (Shanghai Academy of Spaceflight Technology) CCAC group. Its development project was approved in August 2009.

The launcher is approximately 29 m high with a liftoff weight of 103 t. The 1st stage is 3,35m in diameter, the 2nd and 3rd are 2.25m in diameter. The thrust at liftoff is 1200 kN. The reliability of the launcher is 0.98.

Still according to the article, the boosted version of CZ-6 (CZ-6A ??) will make its first flight during the 13th Five Year Plan (2016-2020).

Other sources indicate that CZ-6A will have a 4t payload capacity to 700 km SSO, whereas the today's CZ-6 capability is 500 kg to 700 km SSO.

http://www.jfdaily.com/shizh/bwyc/201509/t20150920_1828654.html

2015/09/21

CZ-6A, CZ-6B, CZ-6C, CZ-6D mods entering national development roadmap. Next mod CZ-6A will make its first flight during the 13th Five Year Plan (2016-2020).

http://www.chinaspaceflight.com/rocket/CZ-6/CZ6-family.html

Total length:29.3 m
Fairing diameter: 2.6 m
Fairing length: 6.145 m

http://bbs.9ifly.cn/forum.php?mod=redirect&goto=findpost&ptid=12833&pid=379633

First stage fueled with LOX and Kerosene and powered by one single YF-100 engine developing 120 tons thrust.

The second stage uses the same fuels with one single YF-115 engine.

The third stage uses conventional propellants powered by a single engine.

http://www.chinanews.com/gn/2015/09-20/7533612.shtml

YF-100 data (for reference only):

Ground level engine

Use: CZ-5 and CZ-7, 3.35 m and 2.25 m diameters boosters engine, CZ-7 first stage core engine, CZ-6 first stage engine.
Staged combustion cycle, liquid oxygen - kerosene engine, enriched pre-ignition.
Ground thrust: 1199.19 kN (122.3 tons)
Ground specific impulse: 2942.0 meters / second (300 seconds)
Vacuum thrust: 1339.48 kN (136.7 tons)
Vacuum specific impulse: 3286.2 meters / second (335 seconds)
Oxygen flow: 296.39 kg / second
Kerosene flow rate: 113.31 kg / second
Total flow rate: 409.70 kg / second
Combustion chamber pressure: 18MPa
Mixing ratio: 2.6
Mixing ratio adjustment range: +/- 10%
Throat area: 1.406 m2
Throat diameter: 1.338 m
Nozzle area ratio: 35
Thrust adjustment: 65% to 100%
Height: 2.991 m
Development: 2000-2012

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Static ground testing

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Static ground testing

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Static ground testing

http://bbs.meyet.com/forum.php?mod=redirect&goto=findpost&ptid=321328&pid=3616067

YF-115 data (for reference only):

Altitude engine

Use: CZ-7 second stage core engine, CZ-6 second stage engine.
Staged combustion cycle, liquid oxygen - kerosene engine, enriched pre-ignition.
Ground thrust: 15 tons
Vacuum Thrust: 18 tons
Thrust adjustment range: 80% to 100%
Vacuum specific impulse: 3349 m / sec (342 seconds)
Combustion chamber pressure: 12MPa
Mixing ratio: 2.5
Mixing ratio adjustment range: +/- 8%
Throat diameter: 0.946 m
Nozzle area ratio: 88
Height: 2.325 m
Development: 2002-2014
Static ground testing: first tested on August 29, 2014

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Static ground testing of four YF-115 engines (CZ-7 second stage)

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Static ground testing of four YF-115 engines (CZ-7 second stage)

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Static ground testing of four YF-115 engines (CZ-7 second stage)

http://www.9ifly.cn/forum.php?mod=viewthread&tid=10063

Third stage is similar to Yuanzheng-1 upper stage engine; it is basically an upper stage

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http://bbs.9ifly.cn/forum.php?mod=redirect&goto=findpost&ptid=12833&pid=379909

Payload adapter

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CZ-6 demonstrator rehearsal rollout

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2000

Launch pad LC16 revealed

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New launch pad

New LC16 rebuild for CZ-6 SLV

Coordinates: 38°50'12.9"N 111°36'21.2"E

https://www.google.com/maps/place/3...3,1501m/data=!3m1!1e3!4m2!3m1!1s0x0:0x0?hl=en
 
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Soheil_Esy

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Part 2

Assembly

2015-09-22

CZ-6 preparation takes 7 days

The rocket remains in the integration area for 4 days; this period is compressible, as is the total preparation time

The transporter vehicle weighs 50t and can provide air conditioning for the rocket and its satellites

The transporter vehicle enters fully autonomous mode, without any human intervention as it reaches 10 m from the launch pad. Mooring and lifting of the rocket are automatic.

The rocket remains between 2-3 days on the launch pad before launch. But for this first launch, the rocket was on the launch pad since September 13, 2015.

http://zhuanti.spacechina.com/n1014805/n1014885/c1036480/content.html

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https://twitter.com/cnspaceflight/status/645373908128927744

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Rollout

On September 13, 2015

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Rollout transfer to launch pad under supervision of a quadcopter drone

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Launch pad LC16

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http://zhuanti.spacechina.com/n1014805/index.html
 
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Cosmic Penguin

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Seems to be a full success. Official news should come very soon...

Amazing the story made it to the state news TV channel just before launch. Here's some CG and launch processing shots of the LM-6:

L61001.jpg


L61002.jpg


L61003.jpg


L61004.jpg


L61005.jpg


L61006.jpg


L61007.jpg
 
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Soheil_Esy

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Part 3

Launch

Launch sequence

T-9 kerosene fueling of the 1st and 2nd stage
T-7h end of kerosene fueling
T-4h LOX fueling of the 1st and 2nd stage
T-2h40m end of LOX fueling of the 2nd stage
T-2h20m end of LOX fueling of the 1st stage
T-15m tower evacuation
T-3m the arm goes down
T-0 ignition
T + 980s start of satellites separation
http://zhuanti.spacechina.com/n1014805/n1014860/c1036366/content.html

Third stage fueling with conventional propellants

24 Oct 2015

CSFTnU7UcAA_1YP.jpg

CSFToTLUcAA2E9P.jpg


https://twitter.com/cnspaceflight/status/657898974154637312

First launch window

Sep 16 17:33:32 UTC 2015

Launch time: UTC 23:00:00 on 2015-09-18

The satellites will separate from rocket at UTC 23:15:14 on 2015-09-18

Keplerian data
Code:
XW-2(CAS-3)
1 99999U               15261.96885740  .00004980   00000-0  28369-3   0
00000
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010

http://amsat.org/pipermail/amsat-bb/2015-September/054848.html

Launch aborted at T-10 Minutes

after problem detected

https://twitter.com/cnspaceflight/status/645076536563904512

Postponed to September 2X, 2015, 07:00 Beijing Time (UTC+8):rolleyes:
praying.gif


http://www.chinaspaceflight.com/rocket/CZ-6/CZ6-first-launch.html

Sat Sep 19 00:28:23 UTC 2015

Short pass, but I monitored XW-2 A, & B on the 00:10utc pass.

Nothing heard on CW , 19K2 or 9k6 telemetry.
Transponder was not expected to be on.

http://amsat.org/pipermail/amsat-bb/2015-September/054884.html
Sat Sep 19 00:54:28 UTC 2015

The launch postponed by one day due to technical reasons, will be at UTC
23:00:00 on 2015-09-19

http://amsat.org/pipermail/amsat-bb/2015-September/054886.html

New XW-2(CAS-3) Keplerian data

Sat Sep 19 01:23:00 UTC 2015

I believe I have figured out keps for a launch 23:00:00 UTC 19 Sept 2015

Code:
CAS-3A
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3B
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3C
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3D
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3E
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3F
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3G
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3H
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010
CAS-3I
1 99999U          15262.96885740  .00004980  00000-0  28369-3    0002
2 99999 097.4712 269.8396 0010382 266.0521 270.6645 15.12847582000010

http://amsat.org/pipermail/amsat-bb/2015-September/054888.html

XW-2(CAS-3) Keplerian data Update

Sat Sep 19 05:13:17 UTC 2015

Code:
XW-2(CAS-3)
1 99999U          15262.96885748  .00004985  00000-0  28395-3 0 00005
2 99999 097.4712 270.8252 0010383 266.0522 270.6644 15.12847565000015

Launch time: UTC 23:00:00 2015-09-19
The satellites will be separated from rocket at UTC 23:15:14 2015-09-19

http://amsat.org/pipermail/amsat-bb/2015-September/054890.html

Sat Sep 19 14:10:56 UTC 2015

I wrote the initial doppler.sqf data for SatPC32.;

Code:
XW-2
1 99999U          15262.96885748  .00004985  00000-0  28395-3 0 00005
2 99999 097.4712 270.8252 0010383 266.0522 270.6644 15.12847565000015

Code:
XW-2,145640,,USB,,,,TLM A
XW-2,145660,,CW,,,,TLM A
XW-2,145675,435040,USB,LSB,REV,0,0,A
XW-2,145705,,USB,,,,TLM B
XW-2,145725,,CW,,,,TLM B
XW-2,145740,435100,USB,LSB,REV,0,0,B
XW-2,145770,,USB,,,,TLM C
XW-2,145790,,CW,,,,TLM C
XW-2,145805,435160,USB,LSB,REV,0,0,C
XW-2,145835,,USB,,,,TLM D
XW-2,145855,,CW,,,,TLM D
XW-2,145870,435220,USB,LSB,REV,0,0,D
XW-2,145890,,USB,,,,TLM E
XW-2,145940,,CW,,,,TLM E
XW-2,145925,435280,USB,LSB,REV,0,0,E
XW-2,145955,,USB,,,,TLM F
XW-2,145975,,CW,,,,TLM F
XW-2,145970,435340,USB,LSB,REV,0,0,F

I hope it helps.

http://amsat.org/pipermail/amsat-bb/2015-September/054891.html

2015-09-19

Satellites radio frequency information

Lexicon:

线性转发器: linear transponder
上行:uplink
下行:downlink
CW信标: CW beacon
遥测: telemetry

Code:
1、 XW-2A:线性转发器:上行:435.030 ‐ 435.050 MHz 下行:145.665 ‐ 145.685 MHz ;CW信标:145.660 MHz;遥测:145.640 MHz9.6/19.2kbps, GMSK

2、 XW-2B:线性转发器:上行:435.090 ‐ 435.110 MHz 下行:145.730 ‐ 145.750 MHz ;CW信标:145.725 MHz;遥测:145.705 MHz9.6/19.2kbps, GMSK

3、 XW-2C:线性转发器:上行:435.150 ‐ 435.170 MHz 下行:145.795 ‐ 145.815 MHz ;CW信标:145.790 MHz;遥测:145.770 MHz9.6/19.2kbps, GMSK

4、 XW-2D:线性转发器:上行:435.210 ‐ 435.230 MHz 下行:145.860 ‐ 145.880 MHz ;CW信标:145.855 MHz;遥测:145.835 MHz9.6/19.2kbps, GMSK

5、 XW-2E:线性转发器:上行:435.270 ‐ 435.290 MHz 下行:145.915 ‐ 145.935 MHz ;CW信标:145.910 MHz;遥测:145.890 MHz9.6kbps, GMSK

6、 XW-2F:线性转发器:上行:435.330 ‐ 435.350 MHz 下行:145.980 ‐ 146.000 MHz ;CW信标:145.975 MHz;遥测:145.955 MHz9.6kbps, GMSK

7、 DCBB:遥测:145.475MHz 9.6kbps, GMSK

8、 LilacSat ‐2 :FM/APRS转发器:上行:144.35MHz;下行:437.200MHz;信标:437.200MHz BPSK/MSK/AFSK 和437.225MHz FSK ;

9、 NUDT‐Phone‐Sat:遥测:437.300MHz9.6kbps, FSK



http://www.pttcn.net/a/zixun/guona/2015/0918/23447.html?bsh_bid=738517274

Second launch window

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Note the lateral symetrical white smoke

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Note the lateral symetrical white smoke

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Successful lift-off

VIDEO

Clearer view on the launch sequence


Longer report with details covering Tiantuo-3 multi-satellites

http://news.cntv.cn/2015/09/20/VIDE1442708460961714.shtml
 
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Soheil_Esy

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Part 4

In orbit


CPSOE3SWcAAldp2.png


7:40 AM - 20 Sep 2015

Singapore 9V1SV station receiving 17 data packages from Lilacsat-2 (紫丁香2号)

2015/09/17

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LilacSat-2 is a low-cost, approx 11kg 20x20x20cm, nano-satellite for education, amateur radio communication and technology demonstration, built by a team of 15 students of HIT. 5 of them are licensed radio amateurs.

LilacSat-2 provides hands-on experience for students who would not otherwise have the opportunity to build flight hardware for a space mission. The training these students gain by working on this project will better prepare them for work in the aerospace industry.

LilacSat-2 carries 4 mission payloads:

1. A V/U amateur radio SDR platform. It can be configured as an FM repeater or an APRS digipeater.It will also provide a VHF CW beacon and UHF 9k6 BPSK telemetry downlink

2. An SDR based multi-band receiver, for reception and decoding of signals from AIS, ADS-B, etc.

3. An FPGA software testing platform.

4. A thermal infrared camera. The lifetime of LilacSat-2 is expected to be 3 to 6 months.

It is expected to launch into a 520x520km orbit with 97 degree inclination together with XW2. More info at http://www.by2hit.net/ and http://www.hit.edu.cn/ **Downlinks on 437.200 MHz for the beacon, 437.225 MHz for the FM/APRS and also uplinks on 145.825 & 145.875 MHz have been coordinated

http://lilacsat.hit.edu.cn/

https://twitter.com/cnspaceflight/status/645381880510984192

Sat Sep 19 23:43:37 UTC 2015

XW-2 (for XiWang2A-2F) (CAS-3) (希望二号A-F小卫星) got into orbit

2015/08/15

Headline Details:

A constellation of nine microsats and nanosats intended to be deployed into a 520km circular or lower elliptical orbits with 97 degree inclinations. Planned launch date is between 5-7th September 2015.Each of the six satellites CAS-3A to CAS-3F will have same amateur radio equipments on board, but operates on different frequencies of 2m band downlink.

● CAS-3A: ● U/V Mode Linear Transponder: 145.675MHz ● CW Telemetry Beacon: 145.660MHz ● AX.25 19.2k Baud GMSK Telemetry: 145.640MHz

● CAS-3B: ● U/V Mode Linear Transponder: 145.740MHz ● CW Telemetry Beacon: 145.725MHz ● AX.25 19.2k Baud GMSK Telemetry: 145.705MHz

● CAS-3C: ● U/V Mode Linear Transponder: 145.805MHz ● CW Telemetry Beacon: 145.790MHz ● AX.25 19.2k Baud GMSK Telemetry: 145.770MHz

● CAS-3D: ● U/V Mode Linear Transponder: 145.870MHz ● CW Telemetry Beacon: 145.855MHz ● AX.25 19.2k Baud GMSK Telemetry: 145.835MHz

● CAS-3E: ● U/V Mode Linear Transponder: 145.925MHz ● CW Telemetry Beacon: 145.910MHz ● AX.25 4.8k Baud GMSK Telemetry: 145.890MHz

● CAS-3F: ● U/V Mode Linear Transponder: 145.990MHz ● CW Telemetry Beacon: 145.975MHz ● AX.25 4.8k Baud GMSK Telemetry: 145.955MHz ● RF Output Power above: ● U/V Mode Linear Transponder: 20dBm ● CW Telemetry Beacon: 17dBm ● AX.25 19.2k Baud FSK Telemetry: 20dBm ● Emission Designator above: ● U/V Mode Linear Transponder: 20K0V8WWF ● CW Telemetry Beacon: 100HA1AAN ● AX.25 19.2k Baud GMSK Telemetry: 30K0F1DCN ● AX.25 4.8k Baud GMSK Telemetry: 16K0F1DCN Other Satellites:

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http://www.amsatuk.me.uk/iaru/formal_detail.php?serialnum=458

Headline Details:

CAMSAT is working closely with DFH Satellite Co. Ltd which is Chinese governmental aerospace contractor to build six satellites and all involved in amateur radio. A U/V mode linear transponder, a two meters CW telemetry beacon and an AX.25 19.2k, 9.6k and 4.8k baud GMSK telemetry downlink will be attached in each of the six satellites, each set of amateur radio equipment will have the same technical characteristics, but operates on different frequencies of 70cm band uplink and 2m band downlink. In addition, CAMSAT is also assisting other three agencies to complete another three satellites.


The nine satellites are described:

CAS-3A: A micro-satellite for atmospheric physics experiments and amateur radio missions. Planned to be 398x398x398mm dimension regular square shape and approx. 25kg mass with three-axis stabilization system. Two daughter satellites CAS-3E and CAS-3F will be piggybacked on top of the satellite.

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CAS-3B, CAS-3C and CAS-3D: Three identical micro-satellites for atmospheric physics experiments and amateur radio missions. each satellite will be 246x246x246mm dimension regular square shape and approx. 10kg mass with three-axis stabilization system.

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CAS-3E and CAS-3F: Two identical Cubesats for amateur radio mission only. Planned to be 116x116x116mm dimension regular square shape and approx. 1.5kg mass. They will be piggybacked on CAS-3A satellite and separated after CAS-3A gets into orbit.

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http://www.chinaspaceflight.com/satellite/xiwang-2/xiwang2A-2F.html


http://amsat.org/pipermail/amsat-bb/2015-September/054901.html

VIDEO

2015-09-20 08:21

TianTuo-3 made of six Smartphone satellites array (国防科技大学天拓三号(TT-3) 手机卫星): one main micro-satellite of 20 kg, one 1 kg Smartphone nano-satellite, four 0.1 kg femto-satellites, forming an array "like hen with chicks", for civilan and military applications.

Main satellite is called Luliang-1(吕梁一号/星载AIS). Its AIS system can improve air navigation and maritime navigation. Phase one and two include the launch of 4 Luliang satellites. After completion of the global array, 16 units will be launched in total. Project started in October 2012. Launch of Luliang-2 scheduled for end 2015 or 2016.

Smartphone satellite is called Zhineng hao (智能号), made from commercial smartphone motherboard and using its operating system.

The four smaller "Stardust" (星尘号, Xing chen hao) femto-satellites are among the tiniest in the world.

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Main micro-satellite Luliang-1

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Zhineng hao nano-satellite of 1 kg with Stardust femto-satellites packed on top

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Main micro-satellite behind; inside the yellow box a femto-satellite with unfolded antenna

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Stardust femto-satellite of 0.1 kg

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Micro-satellites forming a worldwide array

http://news.cntv.cn/2015/09/20/VIDE1442708460798702.shtml
http://www.chinaspaceflight.com/satellite/lvliang/lvliang1.html

VIDEO

http://219.232.160.56/vod/news/sznews2015081407.wmv

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Single engine third stage upper stage releasing Kaituo-1A

2015-08-14

Kaituo-1A(深圳东方红海特的开拓一号卫星) and DCBB(CAS-3G) 2U satellites

Sat A: Kaituo-1A with mass of 130 kg
Sat B: DCBB(CAS-3G) 2U with mass of 3kg

● CAS-3G: ● AX.25 9.6k Baud GMSK Telemetry: 145.475MHz ● AX.25 9.6k Baud GMSK Telemetry: 437.950MHz ●RF Output Power: 23dBm ●Emission Designator: 16K0F2DCN

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http://www.szyj.gov.cn/newsplayer.jsp?isd=70152&type=1




 
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Soheil_Esy

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Part 5

On TV

CCTVNews CGI screen capture

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Third stage upper stage with a single engine clearly visible

http://www.kankanews.com/a/2015-09-20/0037110971.shtml

On the ground

Tracking and telemetry

Sun Sep 20 00:15:19 UTC 2015

Copying CAS-3B,C,D telemetry and CW.
Will try and decode telemetry from recordings.
--
Also copying 3E and F
--
Only had 3 degrees here, but copied CW from a few of them.

https://www.dropbox.com/s/lj1e43q8ktd2qgs/XW-2.mp3?dl=0

http://amsat.org/pipermail/amsat-bb/2015-September/054905.html

Sun Sep 20 00:25:25 UTC 2015

Very good copy on CAS-3 CW beacons on A, B, C, D, E, F. Strong!

http://amsat.org/pipermail/amsat-bb/2015-September/054906.html
Sun Sep 20 00:26:58 UTC 2015

Copied solid CW beacons on all satellites. Transponders on 3G and 3F sounded good.

http://amsat.org/pipermail/amsat-bb/2015-September/054907.html
Sun Sep 20 00:32:12 UTC 2015

Same here in EM34. Copied 3A thru 3F. All sounded good.

http://amsat.org/pipermail/amsat-bb/2015-September/054912.html

Some new TLEs

Sun Sep 20 00:37:57 UTC 2015

Code:
1 99999U              15262.96980399 .00004835 0000-0 27502-3 0 00006
2 99999 097.4579 271.1397 0012633 265.0031 272.1050 15.12881105000010
These will probably need some spacings fixed to work.

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http://amsat.org/pipermail/amsat-bb/2015-September/054910.html

XW-2 Satellite over BKK TH 1108z

Sun Sep 20 12:19:34 UTC 2015

I received CW Beacon From XW-2 during 1108UTC Pass
including CAS-3A, CAS-3B, CAS-3C, and CAS-3D
Max El 72 Degree over Bangkok Thailand

you can see from my video on Youtube:

http://www.amsat.org/pipermail/amsat-bb/2015-September/054925.html



XW-2 Beacons over India

http://www.dk3wn.info/p/wp-content/uploads/2015/09/XW-2-rec0920-181514.mp3

Sun Sep 20 13:09:08 UTC 2015

Received beacons from all the satellites during the 12:43 UTC pass over India recording at http://www.dk3wn.info/p/?p=63906 73
Nitin [VU3TYG]

http://www.amsat.org/pipermail/amsat-bb/2015-September/054928.html

XW-2B ID

Sun Sep 20 13:35:49 UTC 2015

XW-2B is either object 40907 or object 40906.
The third stage of the CZ-6 rocket is object 40899.

---

It now looks like XW-2B is object 40906 and XW-2D is object 40907,
but they are only 3 seconds apart...

The exact launch time of this maiden flight of the new Long March 6 (CZ-6)
rocket was 2015-09-19 at 23:01:14.331 UTC.

http://www.amsat.org/pipermail/amsat-bb/2015-September/054938.html

XW-2 predictions on www.amsat.org

Sun Sep 20 14:38:31 UTC 2015

XW2 predictions are available on
http://www.amsat.org/amsat-new/tools/predict/index.php


For the moment, I arbitrarily picked object 40902 to represent the
entire fleet of 6 spacecraft. As the individual spacecraft are
identified and drift away from each other along the orbital track, the
list will expand to list each one.

http://www.amsat.org/pipermail/amsat-bb/2015-September/054931.html


First 16 Hours of LilacSat-2 and Linux LiveCD for Telemetry Decoding

Sun Sep 20 15:14:06 UTC 2015

During the first 16 hours in orbit, we have received nearly 1000 packets of LilacSat-2 from Harbin (BY2HIT), Shihezi (B0/BY2HIT), Nanjing (BI4ST), Xian (Northwestern Polytechnical University) and Singapore (9V1SV). Many thank to all!


Now we have a Linux LiveCD for telemetry decoding released. It can be downloaded from: http://pan.baidu.com/s/1eQfNsGE


Now we have support for FCDPP, USRP and RTL-SDR. Not hard to edit the GRC flowcharts to support other devices.


It can be burned into a USB stick to boot a computer directly, run from a virtual machine or installed into a hard disk.


User manual also included.


More details: http://lilacsat.hit.edu.cn/

http://www.amsat.org/pipermail/amsat-bb/2015-September/054932.html

24 Sep 2015

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First remote sensing image in the IR band taken by LilasSat-2

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First image with Chinese labels of snowy Mount Changbai (长白山; Hancha: Paektusan) over Manchurian and Korean border, taken on 2015-09-20 09:46:58 UTC

http://lilacsat.hit.edu.cn/?p=339


First pass of XW-2 over Brazil

Sun Sep 20 18:24:16 UTC 2015

Here is my reception report on the first pass of XW-2 over Brazil , today
5:50 AM local time (8:50UTC);

http://www.amsat.org/pipermail/amsat-bb/2015-September/054939.html


[ame="http://www.youtube.com/watch?v=Asyd-QupTZ4"]1040z 23 Sep 15 Pass over THAILAND - YouTube[/ame]

TLE of CZ-6 R/B and 14 satellites

2015-9-23 09:03

Previously 2015-049A designated the upper stage or CZ-6 R/B
New TLE designates CZ-6 R/B as 2015-049Q

2015-049A is now a satellite:

40899/2015-049A,516 X 536(KM) X 97.46°


Code:
2015-049A 
1 40899U 15049A   15265.80329082  .00002511  00000-0  14413-3 0  9995
2 40899  97.4565 273.9130 0014603 262.3689 222.0654 15.13367586   447
2015-049B               
1 40900U 15049B   15265.86918005 -.00001637  00000-0 -88404-4 0  9995
2 40900  97.4550 273.9726 0014481 263.7351 217.9990 15.13200889   448
2015-049C               
1 40901U 15049C   15265.86901831  .00003478  00000-0  19951-3 0  9998
2 40901  97.4645 273.9797 0013187 258.7823 221.2185 15.13150413   443
2015-049D               
1 40902U 15049D   15265.86929550  .00004142  00000-0  23787-3 0  9998
2 40902  97.4498 273.9736 0013315 256.3627 223.4831 15.12992723   441
2015-049E               
1 40903U 15049E   15265.92200377  .00001632  00000-0  96349-4 0  9991
2 40903  97.4576 274.0273 0012655 253.4916 151.8639 15.12854691   454
2015-049F               
1 40904U 15049F   15265.87012825  .00000157  00000-0  12658-4 0  9997
2 40904  97.4585 273.9761 0013673 251.8371 229.3905 15.12677137   436
2015-049G               
1 40905U 15049G   15265.87156565  .00001191  00000-0  73134-4 0  9993
2 40905  97.4531 273.9700 0015215 238.6495 242.2606 15.11900674   442
2015-049H               
1 40906U 15049H   15265.87114735  .00001462  00000-0  88406-4 0  9996
2 40906  97.4574 273.9737 0014603 240.9826 239.9897 15.12126414   431
2015-049J               
1 40907U 15049J   15265.87127495  .00002307  00000-0  13754-3 0  9996
2 40907  97.4552 273.9726 0014133 238.1047 243.0154 15.12076060   431
2015-049K               
1 40908U 15049K   15265.86551965  .00001138  00000-0  70597-4 0  9999
2 40908  97.4659 273.9682 0015460 232.3397 212.8241 15.11625631   433
2015-049L               
1 40909U 15049L   15265.87085800  .00002696  00000-0  15883-3 0  9997
2 40909  97.4581 273.9733 0013859 244.0199 237.8247 15.12365043   437
2015-049M               
1 40910U 15049M   15265.79934875 -.00000064  00000-0  00000+0 0  9994
2 40910  97.4594 273.8981 0015030 239.4546 208.6958 15.11907261   319
2015-049N               
1 40911U 15049N   15265.86319870  .00002687  00000-0  15953-3 0  9994
2 40911  97.4590 273.9648 0014114 239.6208 197.6482 15.12085691   332
2015-049P               
1 40912U 15049P   15265.86831199  .00003395  00000-0  19205-3 0  9999
2 40912  97.4603 273.9772 0015940 236.6722 243.1106 15.13636345   331
2015-049Q               
1 40913U 15049Q   15265.82612359  .00007208  00000-0  17767-3 0  9999
2 40913  97.4162 273.9927 0095009  24.4202  98.3639 15.36246210   327

http://bbs.9ifly.cn/forum.php?mod=redirect&goto=findpost&ptid=12833&pid=380512

2015-9-23 09:15

Code:
[B]LILACSAT-2 (CAS-3H)[/B]               
1 40908U 15049K   15265.13814566  .00002088  00000-0  12638-3 0  9994
2 40908  97.4658 273.2579 0015421 235.2071 214.2057 15.11625876   328
[B]XW-2E (CAS-3E) [/B]              
1 40909U 15049L   15264.81304545 -.00000115  00000-0 -29071-5 0  9992
2 40909  97.4577 272.9393 0013829 247.5115 238.7168 15.12355452   273

http://bbs.9ifly.cn/thread-12833-61-1.html

First images from Kaituo-1A

2015-10-23

In the Arctic Forum Congress held recently, the pioneering Shenzhen Aerospace Dongfanghong Satellite Co. first satellite has become the focus of everyone's attention. The Third Arctic Forum Congress was held in Reykjavik, Iceland, from October 16 to 18. Beijing Normal University Global Change and Earth System Science Research vice president Xiao made a special thematic session presentation to the guests on Arctic climate change research, introducing the remarkable progress made by China micro-nano satellite and cubesat research with special reference to the Shenzhen Dongfanghong Satellite Co., Ltd. He disclosed images taken from the satellite of the Arctic Vilkitski Strait region.

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http://www.chinaspaceflight.com/satellite/addchina-Kaituo1AB.html

Payload fairing debris

CZ-6 rocket payload fairing debris landed in Wushan county, Chongqing, some 870 km from Taiyuan. No hydrazine this time, but houses only several hundred meters away.


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CZ-6 commemoration philatelic souvenir

8 Sep 2015

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Issued on occasion of the CZ-6 launcher's maiden flight with 20 satellites; Shaanxi Aerospace Research Philatelic Association.

https://twitter.com/cnspaceflight/status/641456919069065216
 
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