Author Topic: China launchers Q&A  (Read 52353 times)

Offline Satori

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China launchers Q&A
« on: 12/09/2010 10:08 AM »
A new Q&A thread for the Chinese launchers.

I'm searching for information about the CZ-2D Chang Zheng-2D launch vehicle. The CGWIC gives some figures about this launcher but other sites give other distinctive numbers.

Does anyone has some trustworthy numbers for the CZ-2D vheicle characteristics?

Thanks!
« Last Edit: 12/23/2010 07:55 PM by Satori »

Offline powerplay2009

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Re: China launchers Q&A
« Reply #1 on: 12/09/2010 01:17 PM »
There are two many parameters. Tell me which are the main parameters of your interest. I can dig it out for you.

Offline Satori

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Re: China launchers Q&A
« Reply #2 on: 12/09/2010 01:41 PM »
There are two many parameters. Tell me which are the main parameters of your interest. I can dig it out for you.

The main parameters I have for the CZ-2D are the following. Are they correct?
                                       Stage 1  Stage 2 Vernier engines
Dimeter (m)                3,35   3,35   
Stage length (m)                27,910   10,9   
Mass (kg)                192.700   39.550   
Propolent mass (kg)   183.200   35.550   
Propolent   N2O4/UDMH   N2O4/UDMH   N2O4/UDMH
Engine                             YF-20B   YF-23   4 x YF-25
Força (kN)                2.961,6   742,04   47,1
Specific impulse (m/s)   289   297   282
Spf impulse (sea level) (s)   259   260   260
Burn time (s)                170   295   ???

Mass (kg)      232.250   
Lenth (m)      41,056   
Fairing diameter (m)   3,35   
Fairing length (m)      6,983   
Payload capacity SSO (kg)   1.300   

There is also a streched version of the CZ-2D. What are the main differences?

Offline Salo

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Re: China launchers Q&A
« Reply #3 on: 12/09/2010 04:32 PM »
http://www.sinodefence.com/space/launcher/changzheng2.asp
Quote
The CZ-2D is a two-stage, liquid-propellant launch vehicle designed mainly for Low Earth Orbit (LEO) missions, with an LEO payload of 3,700kg. A total of 10 launches were carried out between 1992 and 2008, all from the Jiuquan Satellite Launch Centre.

The CZ-2D is generally carries UDMH/N2O4 for all stages. The first stage uses a YF-21B motor consisting of four 65,000kg-thrust YF-20 chambers motors with swinging nozzles. The second stage has a YF-24F rocket motor consisting of one 75,000kg-thrust YF-22B main motor with fixed nozzles, and a YF-23F swivelling venire motor with four chambers motors that produce a total thrust of 4,700kg. The launcher also features a McDonnell Douglas (now Boeing Aerospace) PAM-D upper stage providing 66,700 lb of thrust.

The ChangZheng 2D is available in two versions: Type A with a 2.90m-diameter fairing and Type B with a 3.35m-diameter fairing.

Offline Salo

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Offline Salo

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Offline Yarrah

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Re: China launchers Q&A
« Reply #6 on: 12/09/2010 05:57 PM »
Great thread. I have two questions:

1. Is it true that from now on all comsats launched by China will be launched on a CZ 3B/E rocket?

2. Does anyone have any specific information on the CZ 4C's third stage? Like number of chambers, thrust, burn time & lsp? And what are the main differences with the CZ 4B's third stage?
« Last Edit: 12/09/2010 07:56 PM by Yarrah »

Offline Yarrah

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Re: China launchers Q&A
« Reply #7 on: 12/09/2010 06:03 PM »
About the CZ 2D, CGWIC says it has a YF-21C engine on the first stage and YF-24C on the second stage, Sinodefence says YF-21B on the first stage and YF-24F on the second stage. Which one is right?

Offline Salo

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Re: China launchers Q&A
« Reply #8 on: 12/09/2010 07:42 PM »
2. Does anyone have any specific information on the CZ 4C's third stage? Like number of chambers, thrust, burn time & lsp? And what are the main differences with the CZ 4B's third stage?
http://danielmarin.blogspot.com/2010/11/lanzamiento-cz-4c-feng-yun-3b.html
http://danielmarin.blogspot.com/2010/08/lanzamiento-cz-4c-yaogan-10.html
http://www.b14643.de/Spacerockets_1/China/CZ-4/Description/Frame.htm
« Last Edit: 12/09/2010 07:46 PM by Salo »

Offline powerplay2009

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Re: China launchers Q&A
« Reply #9 on: 12/10/2010 02:28 AM »
Satori, you are right. And there is no third stage. But there is one module called ETS,
radius       0.99m
Propolent    HTPB
Engine        SRM
length         1.5m
Force          2744 (N*s/kg)

Offline osiossim

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Re: China launchers Q&A
« Reply #10 on: 12/10/2010 09:15 AM »
About the CZ 2D, CGWIC says it has a YF-21C engine on the first stage and YF-24C on the second stage, Sinodefence says YF-21B on the first stage and YF-24F on the second stage. Which one is right?

CGWIC announcement is right.

Offline Satori

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Re: China launchers Q&A
« Reply #11 on: 12/10/2010 06:38 PM »
I'm looking for CZ-2E images, mainly any images related to the January 25, 1995 Apstar-2 launch failure.

Thanks!

Offline Satori

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Re: China launchers Q&A
« Reply #12 on: 12/11/2010 05:28 PM »
I'm looking for CZ-2E images, mainly any images related to the January 25, 1995 Apstar-2 launch failure.

Thanks!

Found this videos on YouTube... I think that on the second video we can see the CZ-2E (Y1) launch pad abort on March 22, 1992; the January 26th, 1995 CZ-2E (Y6) rocket crash; and the St. Valentins massacre on February 14th, 1996 with the CZ-3B (Y1) launch vehicle.



« Last Edit: 12/11/2010 05:40 PM by Satori »

Offline Satori

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Re: China launchers Q&A
« Reply #13 on: 12/12/2010 05:13 PM »
Is it possible to identify when this two CZ-2C were launched?

Offline go4mars

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Re: China launchers Q&A
« Reply #14 on: 12/24/2010 05:04 AM »
http://www.astronautix.com/lvs/ur700m.htm

Zhang Guitian (Apparently a Chinese "acamedician") was talking at a conference in 2006 referring to Chinese plans to build something on the scale the UR-700M.

Does anyone know more about this/able to verify/dispel it?  Or know where it was discussed on another thread?

Thanks. 
Elasmotherium; hurlyburly Doggerlandic Jentilak steeds insouciantly gallop in viridescent taiga, eluding deluginal Burckle's abyssal excavation.

Offline limen4

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Re: China launchers Q&A
« Reply #15 on: 01/03/2011 07:48 PM »
Is it possible to identify when this two CZ-2C were launched?

Rui, not a definitive identification of the launches. But I found some images which maybe give some hints.
The first image shows maybe the second truck which transports the first stage. A launch vehicle number is seen - Y802302 (?).
The second image is from a philatelic cover which commemorates the first commercial piggyback payload. The brown smoke plume at the first stage seems to correspond with those of the very left image in the launch sequence.
Finally an image from the August 1988 launch.
« Last Edit: 01/03/2011 07:55 PM by limen4 »

Offline panzmead

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CZ-3( ) third stage insulation
« Reply #16 on: 01/14/2011 09:05 PM »
All,

would anyone be able to share any information regarding the (assumed) foam insulation of the cryogenic CZ-3(A thru C) third stage?  Of interest is (a) is it bonded on foam, ala the Ariane 1-4 third stages, or sprayed on foam, ala the Delta IV stages, (b) is it exposed or covered with MLI (as on some Centaur stages), (c) are there any good photos of the foam, perhaps during application, finishing, painting (?), etc., and (d) are there published or known designation(s) and physical characteristics, principally the mass density, of the foam?

If my supposition of foam is incorrect, clarification would be welcome.

Any information is most appreciated,

Phillip Anz-Meador

Offline Stan Black

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Re: China launchers Q&A
« Reply #17 on: 09/06/2011 06:59 PM »
 Are the Chinese rockets still manufactured in two locations; SAST still look after the CZ-4 and CZ-2D? What about the engines. And who makes what for the CZ-3 rockets as both CALT and SAST are involved?

http://www.cgwic.com/Partner/index.html
http://www.globalsecurity.org/wmd/world/china/sast.htm
http://www.globalsecurity.org/wmd/world/china/calt.htm

Offline Liss

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Re: China launchers Q&A
« Reply #18 on: 09/09/2011 07:28 PM »
Stan,
CALT (Beijing) designed and produced CZ-3 third stage (LOX/LH2) while SAST used to build first and second stages.
This message reflects my personal opinion based on open sources of information.

Offline Liss

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Re: China launchers Q&A
« Reply #19 on: 09/09/2011 07:58 PM »
Finally an image from the August 1988 launch.
limen4, that is not the picture of the 1988 launch.
In the 05 Aug 1988 launch the spacecraft was of a Jianbing-1A type, i.e. a longer cylindro-conical one, such as in a well-known 1992 launch with Freja. But in the picture we see a typical conical Jianbing-1.
I've found seven other images of the launch in question (more than any other!) but I still don't know which launch it was.
This message reflects my personal opinion based on open sources of information.

Offline Liss

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Re: China launchers Q&A
« Reply #20 on: 09/09/2011 08:40 PM »
Here is another question on CZ-2C.

My understanding is that there were three basic versions of it:
(1) The initial 190-192 metric ton vehicle in use from 1974 till 1993 (four CZ-2 and eleven CZ-2C), actual payload of 1800-2100 kg;
(2) The Iridium version of 213-214 metric tons flown in 1997-2004 (seven Iridiums, TC-1, TC-2, SY-1 and SY-2) with stretched second stage, quoted payload of 2500-2800 kg;
(3) The current version of 233 metric tons flown since 2004 (10 vehicles) with stretched first stage, actual payload of 3900 kg.

Only one Chinese source gives some data for the current version, http://cn.cgwic.com/LaunchServices/LaunchVehicle/LM2C.html (note fuel load figures in the third row of the table which are different from 143+35 and 143+55 for the first two versions). Yet the difference from the Iridium version is easibly visible in photos at the same Taiyuan pad:

(upper -- 08 Dec 1997) (lower -- 11 Apr 2007)


In the upper photo, first stage from the lower blue ring to the interstage struts is equal to 3.5 levels of service structure, the second stage is another 2.5 levels high and the payload shroud is almost two levels more.

In the lower photo, first stage is definitely four levels high.

Mod Edit: Do not embed images
« Last Edit: 09/11/2011 08:48 PM by Ronsmytheiii »
This message reflects my personal opinion based on open sources of information.

Online Phillip Clark

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Re: China launchers Q&A
« Reply #21 on: 09/10/2011 07:29 AM »
Regarding the information on the link which Igor has provided:   http://cn.cgwic.com/LaunchServices/LaunchVehicle/LM2C.html

First, the launch record omits the launch failure of November 1974.

My understanding has always been that the November 1974 launch failure plus the FSW launches of 1975, 1976 and 1978 all used the original CZ-2 aka CZ-2A launch vehicle, with the 2C only being introduced in 1982.   Note that in Stan Black's listing the 1982 CZ-2C is "Y1", indicating the first flight.

Looking at the CZ-3B entry, I see that the differences between that and the CZ-3B/E are in the strap-on and first stage propellant masses: the second and third stages are identical.
« Last Edit: 09/10/2011 07:30 AM by Phillip Clark »

Offline Liss

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Re: China launchers Q&A
« Reply #22 on: 09/10/2011 08:52 AM »
The November 1974 failure is the known source of controversy :-)
CALT is known to attribute it to CZ-2 and all launches since 1975 to CZ-2C while CASC lists CZ-2C launches from 1982 only -- which makes more sense in my opinion even if the 1982 version differs from 1974/75 only in uprated engines.
I believe Stan Black's list inherits from a long http://www.9ifly.cn/thread-407-1-1.html topic at the Chinese forum www.9ifly.cn. Several CZ-3 numbers are still educated guess AFAIK but others has been confirmed by Chinese sources and documents. Short and full numbers are known for some vehicles -- for example, Sven Granh's FSW-14 was launched by CZ-2C number Y903210 or Y10 for short, and the Y802302 = Y2 vehicle pictured above was intended for 19 Aug 1983 launch.
By the way, we known the Long March 3 name since 1979 but when exactly Long March 1 and Long March 2 names were announced? When did it become known for sure that FB-1 and CZ-2 both existed? I found that both CZ-2 and CZ-2C names were known by January 1986 but when exactly CZ-2C was identified as the two-stage vehicle used in certain FSW launches?
This message reflects my personal opinion based on open sources of information.

Offline input~2

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Re: China launchers Q&A
« Reply #23 on: 09/10/2011 09:13 AM »
Here is another question on CZ-2C.
....
To add to this discussion, here are two tables extracted from CGWIC "LM-2C" leaflets respectively published in 2009 and 2011.
There are indeed differences in the various lengths..

Offline Liss

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Re: China launchers Q&A
« Reply #24 on: 09/10/2011 10:24 AM »
Input~2, thank you for the tables. It's very interesting to see even larger estimate of current CZ-2C launch mass, 245 metric tons. Don't know if this version has been already flown.

As usual, there is conflict within and between the two tables and the plain logic. One meter of CZ-2C tankage length with 3.35 m diameter is equivalent to 8.8 m3 of propellant and -- for UDMH/N2O4 -- to 10.5 tons of load. So when launch mass goes from 233 to 245 metric tons, you may expect stretching the vehicle one meter or so (which is indeed shown in the table) in either stage or both. Again, the first stage load supports the total mass increase but the stage lengths do not conform with other data. It seems that stage length is the less reliable parameter in such tables.
« Last Edit: 09/10/2011 10:27 AM by Liss »
This message reflects my personal opinion based on open sources of information.

Offline limen4

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Re: China launchers Q&A
« Reply #25 on: 09/10/2011 11:28 AM »
Finally an image from the August 1988 launch.
limen4, that is not the picture of the 1988 launch.
In the 05 Aug 1988 launch the spacecraft was of a Jianbing-1A type, i.e. a longer cylindro-conical one, such as in a well-known 1992 launch with Freja. But in the picture we see a typical conical Jianbing-1.
I've found seven other images of the launch in question (more than any other!) but I still don't know which launch it was.

Yes of course there is no guarantee that the image on the philatelic envelope shows really the Aug 5th 1988 launch. But Jianbing-1 (FSW-0) and Jianbing-1A (FSW-1) had the same design. As far as I know, only the camera system was changed for mapping purposes. The new spacecraft design you mentioned was only introduced by Jianbing-1B (FSW-2). In case of Freja a cylindrical adapter was added to the FSW-1 to accommodate the Freja payload.
My conclusion is that the image on the philatelic envelope could show the Aug 5th 1988 launch. I upload images of the FSW-1-payload used for the Aug 5th 1988 launch (a copy from a sticker) and the arrangement of Freja and the corresponding FSW-1 payload. Enclosed the philatelic envelop I also found a (very bad) b/w copy from a Remin Ribao newspaper cutout, which shows the launch on Aug 5th 1988.


Offline Liss

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Re: China launchers Q&A
« Reply #26 on: 09/10/2011 11:37 AM »
limen4, thank you! Now I strongly believe you are correct.
By the way, launch time in Renmin Ribao is given as 16:30 Beijing Summer Time, now abandoned.
« Last Edit: 09/10/2011 12:30 PM by Liss »
This message reflects my personal opinion based on open sources of information.

Offline Stan Black

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Re: China launchers Q&A
« Reply #27 on: 09/10/2011 01:14 PM »
The November 1974 failure is the known source of controversy :-)
CALT is known to attribute it to CZ-2 and all launches since 1975 to CZ-2C while CASC lists CZ-2C launches from 1982 only -- which makes more sense in my opinion even if the 1982 version differs from 1974/75 only in uprated engines.
I believe Stan Black's list inherits from a long http://www.9ifly.cn/thread-407-1-1.html topic at the Chinese forum www.9ifly.cn. Several CZ-3 numbers are still educated guess AFAIK but others has been confirmed by Chinese sources and documents. Short and full numbers are known for some vehicles -- for example, Sven Granh's FSW-14 was launched by CZ-2C number Y903210 or Y10 for short, and the Y802302 = Y2 vehicle pictured above was intended for 19 Aug 1983 launch.
By the way, we known the Long March 3 name since 1979 but when exactly Long March 1 and Long March 2 names were announced? When did it become known for sure that FB-1 and CZ-2 both existed? I found that both CZ-2 and CZ-2C names were known by January 1986 but when exactly CZ-2C was identified as the two-stage vehicle used in certain FSW launches?

http://www.9ifly.cn/thread-407-1-1.html
That is a very good source of information, which I tried to make more accessible to people on this forum.

From what I learnt I found references to CZ-4B Y14 for Haiyang-2.

On that forum CZ-2C 长征二号丙 is also listed with two additional versions: 加长 and 再加长

I’ve re-visited previous post on this forum and I cannot find a fourth version.

Taiyuan
http://forum.nasaspaceflight.com/index.php?topic=7477.msg128652#msg128652
http://forum.nasaspaceflight.com/index.php?topic=12961.msg312760#msg312760
http://forum.nasaspaceflight.com/index.php?topic=16754.msg393895#msg393895

Jiuquan
http://forum.nasaspaceflight.com/index.php?topic=19423.msg502036#msg502036
http://forum.nasaspaceflight.com/index.php?topic=19753.msg514884#msg514884

http://forum.nasaspaceflight.com/index.php?topic=25820.msg767159#msg767159
http://forum.nasaspaceflight.com/index.php?topic=26188.msg785348#msg785348

Offline Liss

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Re: China launchers Q&A
« Reply #28 on: 09/10/2011 02:36 PM »
Found a mention of the 245 ton version in a Chinese source -- Taikong Tansuo 2007 #8. Unfortunately no more details in the text.

http://www.qikan.com.cn/MagDetails/1009-6205/2007/8.html
http://special.cpst.net.cn/19992009/ht/hj/_/241594199.html

Quote
1978年,在长征二号火箭的基础上,经过适应性的技术改进设计,研制成功一种新的运载火箭——长征二号丙。火箭全长约40米,卫星整流罩最大直径3.35米,起飞质量245吨,近地轨道运载能力达到2.5~3.9吨。

Google Translate:

Quote
In 1978, the Long March II rocket, based on adaptive technologies through improved design, developed a new launch vehicle - the Long March II C. Rockets for about 40 meters, the satellite fairing diameter 3.35 m, take-off mass 245 tons, carrying capacity of near-Earth orbit 2.5 to 3.9 t.

Even earlier mention exists in the FSW-19 launch report of 2004 which used for the first time the third CZ-2C version:
http://news.sina.com.cn/o/2004-08-30/05243528856s.shtml

Quote
此次进行发射的“长征二号丙”运载火箭长41.9米,起飞质量245吨。

Quote
The launch of the "Long March II C" carrier rocket length 41.9 m, take-off mass 245 tons.
« Last Edit: 09/10/2011 03:31 PM by Liss »
This message reflects my personal opinion based on open sources of information.

Offline Liss

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Re: China launchers Q&A
« Reply #29 on: 09/10/2011 03:29 PM »
Quote
Yet the difference from the Iridium version is easibly visible in photos at the same Taiyuan pad:

(upper -- 08 Dec 1997) (lower -- 11 Apr 2007)

From the pictures above, I'd said that the shroud and second stage are identical but the first stage is some 2.5 meters longer (and have fins of course).

2.5 meters layer of propellant is some 26 tons of load. Adding tankage mass and fins we'd probably have 2 more tons. Seems to be generally compatible with total mass increase of 213 to 245 tons rather than to 233 tons. More detailed image of the newest vehicle may provide for more accurate estimate.

« Last Edit: 09/10/2011 07:02 PM by Liss »
This message reflects my personal opinion based on open sources of information.

Offline input~2

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Re: China launchers Q&A
« Reply #30 on: 09/10/2011 04:36 PM »
Found a mention of the 245 ton version...
Interestingly, Google gives the following results:
+"长征二号丙"  +"213吨" (CZ-2C/213t)  2207 results
+"长征二号丙"  +"233吨" (CZ-2C/233t)  0 result
+"长征二号丙"  +"245吨" (CZ-2C/245t)  416 results

I am wondering if 233t is not a typo for 213t in the CGWIC litterature ???

CALT has a table for an "improved" version (长征二号丙改进型运载火箭) with a mass of 213 t
http://www.calt.com/cpyfw/yzhj/cp/2009123015071136e9f8.html
(dated 2009-12)
« Last Edit: 09/10/2011 04:45 PM by input~2 »

Offline Stan Black

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Re: China launchers Q&A
« Reply #31 on: 09/10/2011 04:40 PM »
Found a mention of the 245 ton version...
Interestingly, Google gives the following results:
+"长征二号丙"  +"213吨" (CZ-2C/213t)  2207 results
+"长征二号丙"  +"233吨" (CZ-2C/233t)  0 result
+"长征二号丙"  +"245吨" (CZ-2C/245t)  416 results

I am wondering if 233t is not a typo for 213t in the CGWIC litterature ???

CALT has a table for an improved version (长征二号丙改进型运载火箭)with a mass of 213 t
http://www.calt.com/cpyfw/yzhj/cp/2009123015071136e9f8.html

And the CZ-2D is 250t
http://www.spacechina.com/cpyfw_yhxt_yzhj_Details.shtml?recno=60472

Offline input~2

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Re: China launchers Q&A
« Reply #32 on: 09/10/2011 04:51 PM »
And the CZ-2D is 250t
http://www.spacechina.com/cpyfw_yhxt_yzhj_Details.shtml?recno=60472
Here my 2011 CGWIC datasheet gives 249.6t which seems consistent ;)
Only their website gives 232.7t :(
http://cn.cgwic.com/LaunchServices/LaunchVehicle/LM2D.html

with an easy-to-detect typo in this page
http://www.cgwic.com/LaunchServices/LaunchVehicle/LM2D.html
Quote
Lift-off Mass (t)            2961.6kN

Conclusion:
check twice before using CGWIC numbers ;D
 
« Last Edit: 09/10/2011 05:09 PM by input~2 »

Offline Liss

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Re: China launchers Q&A
« Reply #33 on: 09/10/2011 07:06 PM »
It seems that 233 tons migrated from then-2D to 2C :-)
Well, CNSA lists length of the 2004 CZ-2C as 41.947 meters -- http://www.cnsa.gov.cn/n1081/n7529/n7935/11488.html
This message reflects my personal opinion based on open sources of information.

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Re: China launchers Q&A
« Reply #34 on: 09/10/2011 07:44 PM »
For the total length of the 245t version, CGWIC seems once again isolated with its 43m value...

Offline Stan Black

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Re: China launchers Q&A
« Reply #35 on: 09/11/2011 10:19 AM »
Quote
Yet the difference from the Iridium version is easibly visible in photos at the same Taiyuan pad:

(upper -- 08 Dec 1997) (lower -- 11 Apr 2007)

From the pictures above, I'd said that the shroud and second stage are identical but the first stage is some 2.5 meters longer (and have fins of course).

2.5 meters layer of propellant is some 26 tons of load. Adding tankage mass and fins we'd probably have 2 more tons. Seems to be generally compatible with total mass increase of 213 to 245 tons rather than to 233 tons. More detailed image of the newest vehicle may provide for more accurate estimate.



So the 162 fuel load figure, and 213 lift-off mass are misleading?

 
 
Chang Zheng 2C
Stage 1
Propellant
Mass
Stage 2
Propellant
Mass
Total
Lift-off
Mass
 
 
Missions
长征二号丙14335192Jianbing 1
Jianbing 1A
长征二号丙(加长)14355213Shiyan Weixing 1&2
Iridium
Tance
长征二号丙(再加长)17255245 Jianbing 4
Shijian 8
Haiyang 1B
Yaogan Weixing 6
Shijian 11
Huanjing 1
« Last Edit: 09/11/2011 04:57 PM by Stan Black »

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Re: China launchers Q&A
« Reply #36 on: 09/11/2011 10:34 AM »
I think so.
The 172 and 55 ton fuel loads are compatible with durations of engine burns for SJ-11-03 launch which are barely visible in launch center photos.
Stage lengths are beyond repair :-)
This message reflects my personal opinion based on open sources of information.

Offline Stan Black

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Re: China launchers Q&A
« Reply #37 on: 09/11/2011 05:28 PM »
I think so.
The 172 and 55 ton fuel loads are compatible with durations of engine burns for SJ-11-03 launch which are barely visible in launch center photos.
Stage lengths are beyond repair :-)

Found a break down of lengths for the CZ-4A
http://www.space.cetin.net.cn/docs/ht9902/ht990206.htm

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Re: China launchers Q&A
« Reply #38 on: 09/12/2011 02:34 PM »
I think so.
The 172 and 55 ton fuel loads are compatible with durations of engine burns for SJ-11-03 launch which are barely visible in launch center photos.
Stage lengths are beyond repair :-)

Found a break down of lengths for the CZ-4A
http://www.space.cetin.net.cn/docs/ht9902/ht990206.htm

I give up… I too cannot figure out those stage lengths

CZ-2Dhttp://www.space.cetin.net.cn/docs/ht9712/ht971208.htm
CZ-2Ehttp://www.space.cetin.net.cn/docs/ht9801/ht980111.htm
CZ-3Bhttp://www.space.cetin.net.cn/docs/ht9810/ht981014.htm
CZ-4Bhttp://www.space.cetin.net.cn/docs/ht9905/ht990507.htm
« Last Edit: 09/12/2011 02:35 PM by Stan Black »

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Re: China launchers Q&A
« Reply #39 on: 09/14/2011 01:27 AM »
I'm still confused about the  SD, SM and SMA kick stages used for Iridium, Tan Ce and HJ-1A/B - lots of different versions of mass and size out there. One stage has 2620 kg propellant 309 kg dry (described in a paper at IAC 2004) - I gather this is the Tan Ce's SM? One is apparently only 22 kg propellant - is this the SMA?
And the SD had a motor which was 125 kg prop 33 kg dry but probably 550 kg total dry for the stage (rather than just the motor).
 Clarification and confirmation would be welcome.
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Offline Galactic Penguin SST

Re: China launchers Q&A
« Reply #40 on: 01/28/2012 02:20 PM »
This is what I believe the correct pairings of stages for the current versions of Chinese launchers (as of 2012). Note that I'm using the notation first used on the Ariane family to describe the amount of propellant on each stage when fully fueled. The items in bold are those that are uncertain. Any comments?

1st stage of CZ-2C/CZ-3A/CZ-3B(original)/CZ-3C = L172
1st stage of  CZ-3B/E / CZ-2F = L186
1st stage of  CZ-2D / CZ-4B / CZ-4C = L183
2nd stage of CZ-3A = L30
2nd stage of CZ-4B / CZ-4C = L35
2nd stage of CZ-3B / CZ-3B/E / CZ-3C = L45
2nd stage of CZ-2C / CZ-2D = L55
2nd stage of CZ-2F = L86
3rd stage of CZ-3A / CZ-3B / CZ-3B/E / CZ-3C = H18
3rd stage of CZ-4B / CZ-4C = L12
Booster stage of CZ-3B/E / CZ-2F (pre-TG-1) / CZ-3C (with propellant offload?)= L40
Booster stage of CZ-3B (original) = L38
Booster stage of CZ-2F (2011 version) = L4?
« Last Edit: 01/28/2012 03:17 PM by Galactic Penguin SST »
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Offline Galactic Penguin SST

Re: China launchers Q&A
« Reply #41 on: 01/29/2012 09:57 AM »
This is what I believe the correct pairings of stages for the current versions of Chinese launchers (as of 2012). Note that I'm using the notation first used on the Ariane family to describe the amount of propellant on each stage when fully fueled. The items in bold are those that are uncertain. Any comments?

1st stage of CZ-2C/CZ-3A/CZ-3B(original)/CZ-3C = L172
1st stage of  CZ-3B/E / CZ-2F = L186
1st stage of  CZ-2D / CZ-4B / CZ-4C = L183
2nd stage of CZ-3A = L30
2nd stage of CZ-4B / CZ-4C = L35
2nd stage of CZ-3B / CZ-3B/E / CZ-3C = L45
2nd stage of CZ-2C / CZ-2D = L55
2nd stage of CZ-2F = L86
3rd stage of CZ-3A / CZ-3B / CZ-3B/E / CZ-3C = H18
3rd stage of CZ-4B / CZ-4C = L12
Booster stage of CZ-3B/E / CZ-2F (pre-TG-1) / CZ-3C (with propellant offload?)= L40
Booster stage of CZ-3B (original) = L38
Booster stage of CZ-2F (2011 version) = L4?


Following my earlier post, I've asked the same question on a Chinese forum. Here's the answer:

CZ-2C (since 2004): L172+L55
CZ-2D (since 2003): L182+L53
CZ-2F (since 1999): 4xL41+L186+L84
CZ-2F/G (since 2011): 4xL45+L186+L84
CZ-3A: L172+L30+H18
CZ-3B (since 1996): 4xL38+L172+L45+H18
CZ-3B/E (since 2007): 4xL41+L186+L45+H18
CZ-3C (original design): 2xL38+L172+L45+H18
CZ-3C (since 2008): 2xL41+L186+L45+H18
CZ-4B/CZ-4C: L182+L34+L14

Source
Chinese spaceflight is a cosmic riddle wrapped in a galactic mystery inside an orbital enigma... - (not) Winston Churchill

Offline Satori

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Re: China launchers Q&A
« Reply #42 on: 01/29/2012 12:17 PM »
Very interesting! Thank you Galactic!

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Re: China launchers Q&A
« Reply #43 on: 02/01/2012 08:12 AM »
 :) significant progress made on CZ-5 project within the first week of Chinese Lunar Calendar Year of Dragon......Although low quality screen shots from CNTV again......
« Last Edit: 02/01/2012 08:14 AM by Victory O »

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Re: China launchers Q&A
« Reply #44 on: 02/16/2012 04:31 AM »
:) significant progress made on CZ-5 project within the first week of Chinese Lunar Calendar Year of Dragon......Although low quality screen shots from CNTV again......

Here is link on similar report - maybe same, dont know(somewhat shortened and without graphics)
http://newscontent.cctv.com/news.jsp?fileId=129307

Also, is the rocket on the right (on infographics) LM-5? I think so, according to numbers, but not sure. Will it use liquid propellant boosters, or not yet known?

Offline Galactic Penguin SST

Re: China launchers Q&A
« Reply #45 on: 10/07/2013 04:19 AM »
Someone has posted a Chinese paper that resolves all configuration discrepancies between the different rockets of the CZ-3A series.  :)

Basically:

CZ-3A - just the one sub-variant
CZ-3B:
standard version - the original CZ-3B as flown in 1996, with standard length first stage and boosters, uses the 4.0 m diameter 4000F fairing
CZ-3B/G1 - standard version CZ-3B with the 3.7 m diameter 3700Z dual-payload fairing, only used for the dual COMPASS MEO launches in 2012
CZ-3B/G2 - the original enhanced CZ-3B, with lengthened first stage and boosters, uses the 4.0 m diameter 4000F fairing, first flown in 2007
CZ-3B/G3 - enhanced CZ-3B with the 4.2 diameter 4200F fairing
CZ-3B/G2 and G3 corresponds to what we call the "CZ-3B/E".

CZ-3C - currently just the one sub-variant, with standard length first stage and boosters, uses the 4.0 m diameter 4000F fairing (contradictory to what I said earlier, the CZ-3C as flown today do not use the lengthened first stage and boosters , but see below)

The problems with the different stage configurations (e.g. the pad at Xichang requires mating/de-mating of electric cables and gas ducts on the umbilical arms every time between launches of a CZ-3B/E and a CZ-3C) means that there's a need to standardize the launcher configurations. The "standard length" boosters will be phased out in the near future, leaving these mainstay sub-variants:

CZ-3B/G2 (GTO capability 5.5 tonnes)
CZ-3B/G3 (GTO capability 5.4 tonnes)
CZ-3C/G2 ("CZ-3C/E", or CZ-3B/G2 minus two boosters)  (GTO capability 3.9 tonnes)

plus these special variants:

CZ-3B/G3Z - enhanced CZ-3B with the 4.2 m diameter 4200Z fairing and extra RCS tanks and thrusters on the 3rd stage, probably for extra-long coast missions. May debut on the Chang'e 3 launch later this year. GTO capability 5.2 tonnes.
CZ-3C/G3Z - CZ-3B/G2 minus two boosters. GTO capability 3.7 tonnes.
CZ-3B/YZ-1 - enhanced CZ-3B with the 4.2 m diameter 4200Z fairing and the planned GEO direct insertion upper stage (probably the one using RP-1/H2O2 fuel as exhibited in various aerospace exhibits over the past several years), will be used for future COMPASS system launches
CZ-3C/YZ-1 - CZ-3B/YZ-1 minus two boosters, will be used for future COMPASS system launches

Maybe someone can help to check which launch uses the sub-variants as described above?  ;)




 
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Offline russianhalo117

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Re: China launchers Q&A
« Reply #46 on: 10/08/2013 03:18 PM »
Someone has posted a Chinese paper that resolves all configuration discrepancies between the different rockets of the CZ-3A series.  :)

Basically:

CZ-3A - just the one sub-variant
CZ-3B:
standard version - the original CZ-3B as flown in 1996, with standard length first stage and boosters, uses the 4.0 m diameter 4000F fairing
CZ-3B/G1 - standard version CZ-3B with the 3.7 m diameter 3700Z dual-payload fairing, only used for the dual COMPASS MEO launches in 2012
CZ-3B/G2 - the original enhanced CZ-3B, with lengthened first stage and boosters, uses the 4.0 m diameter 4000F fairing, first flown in 2007
CZ-3B/G3 - enhanced CZ-3B with the 4.2 diameter 4200F fairing
CZ-3B/G2 and G3 corresponds to what we call the "CZ-3B/E".

CZ-3C - currently just the one sub-variant, with standard length first stage and boosters, uses the 4.0 m diameter 4000F fairing (contradictory to what I said earlier, the CZ-3C as flown today do not use the lengthened first stage and boosters , but see below)

The problems with the different stage configurations (e.g. the pad at Xichang requires mating/de-mating of electric cables and gas ducts on the umbilical arms every time between launches of a CZ-3B/E and a CZ-3C) means that there's a need to standardize the launcher configurations. The "standard length" boosters will be phased out in the near future, leaving these mainstay sub-variants:

CZ-3B/G2 (GTO capability 5.5 tonnes)
CZ-3B/G3 (GTO capability 5.4 tonnes)
CZ-3C/G2 ("CZ-3C/E", or CZ-3B/G2 minus two boosters)  (GTO capability 3.9 tonnes)

plus these special variants:

CZ-3B/G3Z - enhanced CZ-3B with the 4.2 m diameter 4200Z fairing and extra RCS tanks and thrusters on the 3rd stage, probably for extra-long coast missions. May debut on the Chang'e 3 launch later this year. GTO capability 5.2 tonnes.
CZ-3C/G3Z - CZ-3B/G2 minus two boosters. GTO capability 3.7 tonnes.
CZ-3B/YZ-1 - enhanced CZ-3B with the 4.2 m diameter 4200Z fairing and the planned GEO direct insertion upper stage (probably the one using RP-1/H2O2 fuel as exhibited in various aerospace exhibits over the past several years), will be used for future COMPASS system launches
CZ-3C/YZ-1 - CZ-3B/YZ-1 minus two boosters, will be used for future COMPASS system launches

Maybe someone can help to check which launch uses the sub-variants as described above?  ;)
We should create a pinned topic that lists all of China's launchers (Past, Present, and Future) with their associated launch pads so that way people do not have to keep asking in a new topic every time everyone forgets that one exists.

Offline Satori

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Re: China launchers Q&A
« Reply #47 on: 10/08/2013 06:35 PM »
Someone has posted a Chinese paper that resolves all configuration discrepancies between the different rockets of the CZ-3A series.  :)

Basically:

CZ-3A - just the one sub-variant
CZ-3B:
standard version - the original CZ-3B as flown in 1996, with standard length first stage and boosters, uses the 4.0 m diameter 4000F fairing
CZ-3B/G1 - standard version CZ-3B with the 3.7 m diameter 3700Z dual-payload fairing, only used for the dual COMPASS MEO launches in 2012
CZ-3B/G2 - the original enhanced CZ-3B, with lengthened first stage and boosters, uses the 4.0 m diameter 4000F fairing, first flown in 2007
CZ-3B/G3 - enhanced CZ-3B with the 4.2 diameter 4200F fairing
CZ-3B/G2 and G3 corresponds to what we call the "CZ-3B/E".

CZ-3C - currently just the one sub-variant, with standard length first stage and boosters, uses the 4.0 m diameter 4000F fairing (contradictory to what I said earlier, the CZ-3C as flown today do not use the lengthened first stage and boosters , but see below)

The problems with the different stage configurations (e.g. the pad at Xichang requires mating/de-mating of electric cables and gas ducts on the umbilical arms every time between launches of a CZ-3B/E and a CZ-3C) means that there's a need to standardize the launcher configurations. The "standard length" boosters will be phased out in the near future, leaving these mainstay sub-variants:

CZ-3B/G2 (GTO capability 5.5 tonnes)
CZ-3B/G3 (GTO capability 5.4 tonnes)
CZ-3C/G2 ("CZ-3C/E", or CZ-3B/G2 minus two boosters)  (GTO capability 3.9 tonnes)

plus these special variants:

CZ-3B/G3Z - enhanced CZ-3B with the 4.2 m diameter 4200Z fairing and extra RCS tanks and thrusters on the 3rd stage, probably for extra-long coast missions. May debut on the Chang'e 3 launch later this year. GTO capability 5.2 tonnes.
CZ-3C/G3Z - CZ-3B/G2 minus two boosters. GTO capability 3.7 tonnes.
CZ-3B/YZ-1 - enhanced CZ-3B with the 4.2 m diameter 4200Z fairing and the planned GEO direct insertion upper stage (probably the one using RP-1/H2O2 fuel as exhibited in various aerospace exhibits over the past several years), will be used for future COMPASS system launches
CZ-3C/YZ-1 - CZ-3B/YZ-1 minus two boosters, will be used for future COMPASS system launches

Maybe someone can help to check which launch uses the sub-variants as described above?  ;)
We should create a pinned topic that lists all of China's launchers (Past, Present, and Future) with their associated launch pads so that way people do not have to keep asking in a new topic every time everyone forgets that one exists.

Copy that! That's a good idea! I'll work on it. All help will be welcomed!

Offline Dante80

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Re: China launchers Q&A
« Reply #48 on: 11/03/2016 02:48 PM »
With the second LM-11 launch possibly coming in this month, I wanted to look up some more information about the LV. The result was pitiful. Could the limited publicity have anything to do with the LV possibly having technology and part commonalities with the DF-41 ballistic missile which is still under active development?
« Last Edit: 11/03/2016 02:49 PM by Dante80 »

Offline edkyle99

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Re: China launchers Q&A
« Reply #49 on: 11/03/2016 03:03 PM »
With the second LM-11 launch possibly coming in this month, I wanted to look up some more information about the LV. The result was pitiful. Could the limited publicity have anything to do with the LV possibly having technology and part commonalities with the DF-41 ballistic missile which is still under active development?
I believe that CZ-11 may be based on the DF-31 series solid fuel ballistic missile already in China's inventory.  The canister used to launch CZ-11 was similar to launch canisters used by the road-mobile DF-31A. 
http://www.spacelaunchreport.com/cz11.html

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Offline Dante80

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Re: China launchers Q&A
« Reply #50 on: 11/03/2016 03:57 PM »
That was my first thought too (DF-41 is also much bigger than it). Thanks for the prompt reply.

Offline jcm

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Re: China launchers Q&A
« Reply #51 on: 12/18/2016 07:22 AM »
http://build.whir.net/htkg/index_23.aspx  shows the new KZ-11 rocket (there's even a putative link to a user
manual but it's a dead link...)
The rocket is 2.2m diameter, the same as the DF-3/CZ-1 and as the CZ-7 strapons. But those are CALT products I believe, and I expected the KZ-11 to be a CASIC product (as opposed to CALT's CZ-11) since the marketer Expace is a CASIC subsidiary.

Anyone got an idea what the KZ-11 is based on?

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Re: China launchers Q&A
« Reply #52 on: 12/18/2016 12:36 PM »
it took me a while, but I managed to download the KZ-1 user manual
« Last Edit: 12/18/2016 01:20 PM by plutogno »

Offline Galactic Penguin SST

Re: China launchers Q&A
« Reply #53 on: 12/18/2016 12:39 PM »
http://build.whir.net/htkg/index_23.aspx  shows the new KZ-11 rocket (there's even a putative link to a user
manual but it's a dead link...)
The rocket is 2.2m diameter, the same as the DF-3/CZ-1 and as the CZ-7 strapons. But those are CALT products I believe, and I expected the KZ-11 to be a CASIC product (as opposed to CALT's CZ-11) since the marketer Expace is a CASIC subsidiary.

Anyone got an idea what the KZ-11 is based on?

......and I believe KZ-11 is all solid as well so nothing to do with the rockets above.  ;)
Chinese spaceflight is a cosmic riddle wrapped in a galactic mystery inside an orbital enigma... - (not) Winston Churchill

Offline jcm

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Re: China launchers Q&A
« Reply #54 on: 12/18/2016 03:18 PM »
http://build.whir.net/htkg/index_23.aspx  shows the new KZ-11 rocket (there's even a putative link to a user
manual but it's a dead link...)
The rocket is 2.2m diameter, the same as the DF-3/CZ-1 and as the CZ-7 strapons. But those are CALT products I believe, and I expected the KZ-11 to be a CASIC product (as opposed to CALT's CZ-11) since the marketer Expace is a CASIC subsidiary.

Anyone got an idea what the KZ-11 is based on?

......and I believe KZ-11 is all solid as well so nothing to do with the rockets above.  ;)

Ah, good point. So to rephrase the question, it seems unlikely that a 2.2m-diameter all-solid launch vehicle ISN'T
based on a military missile. But I'm not aware of a comparable diameter Chinese solid missile except DF-31/DF-41
which I understand is a CALT/ARMT product.
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Offline Galactic Penguin SST

Re: China launchers Q&A
« Reply #55 on: 12/18/2016 03:44 PM »
http://build.whir.net/htkg/index_23.aspx  shows the new KZ-11 rocket (there's even a putative link to a user
manual but it's a dead link...)
The rocket is 2.2m diameter, the same as the DF-3/CZ-1 and as the CZ-7 strapons. But those are CALT products I believe, and I expected the KZ-11 to be a CASIC product (as opposed to CALT's CZ-11) since the marketer Expace is a CASIC subsidiary.

Anyone got an idea what the KZ-11 is based on?

......and I believe KZ-11 is all solid as well so nothing to do with the rockets above.  ;)

Ah, good point. So to rephrase the question, it seems unlikely that a 2.2m-diameter all-solid launch vehicle ISN'T
based on a military missile. But I'm not aware of a comparable diameter Chinese solid missile except DF-31/DF-41
which I understand is a CALT/ARMT product.

It's probably a new design, especially since IIRC it uses carbon fiber casings (which reminds me that I need to translate all relevant materials on the KZ series to here soon....sigh).
Chinese spaceflight is a cosmic riddle wrapped in a galactic mystery inside an orbital enigma... - (not) Winston Churchill

Offline zotiraki

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Re: China launchers Q&A
« Reply #56 on: 01/17/2017 02:56 PM »
I'm looking for cost data on Chinese launch vehicles.  Anybody have some reputable numbers or a good source?  I have a 2012 source from this forum
(at https://www.nasaspaceflight.com/2012/09/chinese-long-march-2d-launches-vrss-1/)
and a 2013 cost of $70M for a CZ-3B (SpaceNews website, "China Great Wall Reaffirms Commitment to $70 Million Long March Launches"). 
Also have a $10M target cost for KZ-11 from https://www.chinaspaceflight.com/rocket/KZ-11/KZ-11.html
The rest eludes me.  Any help would be appreciated.   

Offline zzabur

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Re: China launchers Q&A
« Reply #57 on: 01/18/2017 07:11 AM »
This article has information about various Chinese launchers, including new CZ-9 (see page 4)
http://jdse.bit.edu.cn/sktcxbcn/ch/reader/create_pdf.aspx?file_no=20160403&flag=1&journal_id=sktcxbcn&year_id=2016

The second author (Long Lehao) was the chief designer of CZ-5, so information here is very credible.

Offline Galactic Penguin SST

Re: China launchers Q&A
« Reply #58 on: 01/18/2017 08:52 AM »
This article has information about various Chinese launchers, including new CZ-9 (see page 4)
http://jdse.bit.edu.cn/sktcxbcn/ch/reader/create_pdf.aspx?file_no=20160403&flag=1&journal_id=sktcxbcn&year_id=2016

The second author (Long Lehao) was the chief designer of CZ-5, so information here is very credible.

Heh, I saw that yesterday and I still don't have time to summarize it! I'll do that later today. ;)
Chinese spaceflight is a cosmic riddle wrapped in a galactic mystery inside an orbital enigma... - (not) Winston Churchill

Offline Moon Rabbit

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Re: China launchers Q&A
« Reply #59 on: 10/19/2017 03:35 AM »
Need help with regards to reading the thread in the sticky https://forum.nasaspaceflight.com/index.php?topic=30673.0

There is a list of orbital launches there. Figured out most of the fields (please correct me if wrong) except the two fields coloured red. What does those two fields represent? I guess the second one is the launch timing, but what is the format...can't figure it out.

<sequence> <(99-99)> - <launch vehicle> <(factory serial no.)> - <launch date> <(9999:99.999)> - <launch site>, <launch pad> - <payload>

Btw, the (factory serial no.) is something i just made up. Another thread describe this as a factory number/serial number. What would be the correct descriptor for this number?

.
.
2015

205 (07-63) - CZ-3C/YZ-1 (Y11/Y1) - March 30 (1352:30.598) - XSLC, LC2 - Beidou-3 I1 (BDS I1-S)
206 (05-46) - CZ-4C (Y30) - June 26 (0622:043.731) - TSLC, LC9 - GF-8
207 (07-64) - CZ-3B/YZ-1 (Y26/Y2) - July 25 (1229:04.411) - XSLC, LC2 - Beidou-3 M1-S (Beidou-18); Beidou-3 M2-S (Beidou-19)
208 (07-66) - CZ-3B/G2 (Y32) - September 12 (1542:04.418) - XSLC, LC2 - Tongxin Jishu Shiyan Weixing-1
209 - CZ-2D (Y21) - September 14 (0442) - JSLC, LC43/603 - Gaofen-9

The Mercury Seven - Carpenter, Cooper, Glenn, Grissom, Schirra, Shepard, Slayton. “Somewhere, something incredible is waiting to be known.” - Carl Sagan

Offline Stan Black

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Re: China launchers Q&A
« Reply #60 on: 10/19/2017 06:59 PM »
Need help with regards to reading the thread in the sticky https://forum.nasaspaceflight.com/index.php?topic=30673.0

There is a list of orbital launches there. Figured out most of the fields (please correct me if wrong) except the two fields coloured red. What does those two fields represent? I guess the second one is the launch timing, but what is the format...can't figure it out.

<sequence> <(99-99)> - <launch vehicle> <(factory serial no.)> - <launch date> <(9999:99.999)> - <launch site>, <launch pad> - <payload>

Btw, the (factory serial no.) is something i just made up. Another thread describe this as a factory number/serial number. What would be the correct descriptor for this number?

.
.
2015

205 (07-63) - CZ-3C/YZ-1 (Y11/Y1) - March 30 (1352:30.598) - XSLC, LC2 - Beidou-3 I1 (BDS I1-S)
206 (05-46) - CZ-4C (Y30) - June 26 (0622:043.731) - TSLC, LC9 - GF-8
207 (07-64) - CZ-3B/YZ-1 (Y26/Y2) - July 25 (1229:04.411) - XSLC, LC2 - Beidou-3 M1-S (Beidou-18); Beidou-3 M2-S (Beidou-19)
208 (07-66) - CZ-3B/G2 (Y32) - September 12 (1542:04.418) - XSLC, LC2 - Tongxin Jishu Shiyan Weixing-1
209 - CZ-2D (Y21) - September 14 (0442) - JSLC, LC43/603 - Gaofen-9



http://forum.nasaspaceflight.com/index.php?topic=36645.msg1320775#msg1320775

Offline russianhalo117

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Re: China launchers Q&A
« Reply #61 on: 10/20/2017 02:46 AM »
Need help with regards to reading the thread in the sticky https://forum.nasaspaceflight.com/index.php?topic=30673.0

There is a list of orbital launches there. Figured out most of the fields (please correct me if wrong) except the two fields coloured red. What does those two fields represent? I guess the second one is the launch timing, but what is the format...can't figure it out.

<sequence> <(99-99)> - <launch vehicle> <(factory serial no.)> - <launch date> <(9999:99.999)> - <launch site>, <launch pad> - <payload>

Btw, the (factory serial no.) is something i just made up. Another thread describe this as a factory number/serial number. What would be the correct descriptor for this number?

.
.
2015

205 (07-63) - CZ-3C/YZ-1 (Y11/Y1) - March 30 (1352:30.598) - XSLC, LC2 - Beidou-3 I1 (BDS I1-S)
206 (05-46) - CZ-4C (Y30) - June 26 (0622:043.731) - TSLC, LC9 - GF-8
207 (07-64) - CZ-3B/YZ-1 (Y26/Y2) - July 25 (1229:04.411) - XSLC, LC2 - Beidou-3 M1-S (Beidou-18); Beidou-3 M2-S (Beidou-19)
208 (07-66) - CZ-3B/G2 (Y32) - September 12 (1542:04.418) - XSLC, LC2 - Tongxin Jishu Shiyan Weixing-1
209 - CZ-2D (Y21) - September 14 (0442) - JSLC, LC43/603 - Gaofen-9


First field you question: The entry format for Chinese Launch authorization code as issued by the Launch Control Centre
Second field you question: The entry format for the full launch time minus the Day. International precise short time format is:
Julian Day or JDay (000 to 366) then Hour (00 to 23) then Minute (00 to 59) then Second (00 to 59) then Millisecond (000 to 999) Then ZULU Time (UTC) or LOCAL Time.
That is DDD:HH:MM:SS.MS ZULU or JD: 000:00:00:00.000 ZULU (alternate precise short format is 000:0000:00.000 ZULU).
« Last Edit: 10/20/2017 04:31 PM by russianhalo117 »

Offline Moon Rabbit

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Re: China launchers Q&A
« Reply #62 on: 10/20/2017 01:56 PM »
Thank you.
The Mercury Seven - Carpenter, Cooper, Glenn, Grissom, Schirra, Shepard, Slayton. “Somewhere, something incredible is waiting to be known.” - Carl Sagan

Offline Liss

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Re: China launchers Q&A
« Reply #63 on: 11/08/2017 06:23 PM »
My browser alarms me that the 9ifly.cn forum is now regarded as a Reported Attack Page. Is there a real threat?
This message reflects my personal opinion based on open sources of information.

Online Skyrocket

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Re: China launchers Q&A
« Reply #64 on: 11/08/2017 06:52 PM »
My browser alarms me that the 9ifly.cn forum is now regarded as a Reported Attack Page. Is there a real threat?

Likely yes. I have checked the site with Sucuri, which confirms, that it has been compromised and could be harmful:
https://sitecheck.sucuri.net/results/9ifly.cn/

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