Author Topic: LIVE: Proton-M launch with Yamal-402 satellite - December 8, 2012 (1313UTC)  (Read 65535 times)

Online Galactic Penguin SST

Apparently the Russians now blame the failure on a turbopump bearing destruction during the final burn.

http://en.rian.ru/science/20121225/178385673.html

How frequent does that happen before in rocket engine flights?
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Offline akula2

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a) Any update on Yamal-402 satellite? I mean, reduction from 15 to 11 years due to use of its fuel. Is this confirmed? Or drastically down to even more (say 8 or 9 years).

b) Anyone know how to compute RoI on Satellites? At least rough estimate will do.

Online smoliarm

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Apparently the Russians now blame the failure on a turbopump bearing destruction during the final burn.

http://en.rian.ru/science/20121225/178385673.html

How frequent does that happen before in rocket engine flights?

Yes, "Kommersant" newspaper confirmed this yesterday (in Russian)

http://www.kommersant.ru/doc-y/2097660

and gave more details:
= The Kommersant's source in the investigation board confirmed the engine (C5.98) failure;
= the board believes that turbopump bearing destruction was the most probable cause;
= Turbopump developer and manufacturer ("КБ Химмаш") will conduct testing of all its turbopumps (that's how the put it in article - ALL);
= two coming launches with Briz-M - Satmex-8 and Anik G1 - are currently postponed till the end of testings;

Also, Kommersant's analyst, Ivan Sofronov noted, that this is not the first case of turbopump bearing destruction. In Feb 2006, Briz-M failed to deploy Arabsat-4A, later the failure was attributed to the bearing destruction, and "КБ Химмаш" concurred with this conclusion.

Offline Prober

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any change in bearing suppliers?

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Offline Chris Bergin

ILS presser:

INVESTIGATION INTO PROTON LAUNCH ANOMALY CONTINUES AS ROOT CAUSE IS BEING EVALUATED

 

December 27, 2012- The Russian Commission, convened by Khrunichev, continues its investigation and is preparing a report concerning the root cause of the December 8th ILS Proton launch anomaly with the Yamal 402 satellite. Various root cause scenarios are being evaluated  prior to the issuance of a final conclusive report.

 

The anomaly occurred during the 4th and final burn of the Breeze M engine during a planned 9 hour and 15 minute mission. The 4th burn ended about four minutes early and the spacecraft was subsequently separated. The spacecraft, built by Thales Alenia Space for Russian satellite operator, Gazprom Space Systems, was successfully maneuvered to its orbital position and has started in-orbit tests.

 

ILS has formed a Failure Review Oversight Board (FROB) in serial process at the conclusion of the Russian Commission. The FROB will review the Commission’s final report and corrective action plan, in accordance with U.S. and Russian government export control regulations.  The FROB will begin in Moscow after the report is issued and consists of ILS customers, industry subject experts, and insurance industry representatives. The FROB will provide an independent review of the investigation, root cause and corrective actions of the Russian Commission required prior to return to commercial flight.  After the conclusion of the FROB, the FROB report will be briefed to ILS customers and the launch insurance industry.

 

Additional information will be provided as it becomes available.

 

 

About ILS and Khrunichev

ILS is a leading launch services provider for global satellite operators and offers a complete array of services and support, from contract signing through mission management and on-orbit delivery.  ILS has exclusive rights to market the Proton vehicle to commercial satellite operators worldwide and is a U.S. company headquartered in Reston, VA., near Washington, D.C.  For more information, visit www.ilslaunch.com.

 

Khrunichev, which holds the majority interest in ILS, is one of the cornerstones of the Russian space industry. Khrunichev manufactures the Proton system and is developing the Angara launch system. The Proton launches from facilities at the Baikonur Cosmodrome in Kazakhstan, and has a heritage of more than 380 missions since 1965. Khrunichev includes, among its branches, a number of key manufacturers of launch vehicle and spacecraft components in Moscow and in other cities of the Russian Federation.  For more information, visit www.khrunichev.com.

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Offline akula2

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Also, Kommersant's analyst, Ivan Sofronov noted, that this is not the first case of turbopump bearing destruction. In Feb 2006, Briz-M failed to deploy Arabsat-4A, later the failure was attributed to the bearing destruction, and "КБ Химмаш" concurred with this conclusion.
I don't discount this at all. We have loads of bad-quality spares experience as well as huge project delays...

= the board believes that turbopump bearing destruction was the most probable cause;
=  Turbopump developer and manufacturer ("КБ Химмаш") will conduct testing  of all its turbopumps (that's how the put it in article - ALL);
If  that's true then Medvedev should have penalized them by now. I don't get why the delay. Perhaps it's  time for the Russian President to set the ball rolling...

Offline Chris Bergin

ILS:

ROSCOSMOS MANAGEMENT RELEASES INVESTIGATIVE COMMISSION’S REPORT
ON PROTON LAUNCH ANOMALY
TO KHRUNICHEV STATE RESEARCH AND SPACE PRODUCTION CENTER

January 11, 2012- Roscosmos management has reviewed and approved the report provided by the Russian working group investigating the Proton launch anomaly during the Yamal 402 mission and have provided the report to Khrunichev State Research and Space Production Center (Khrunichev).The findings on the identified most probable root cause of the anomaly and the required corrective actions will be released to ILS after the report clears Russian security during the week of January 21st.

 

The Russian working group, convened by Roscosmos, included independent experts from TsNIIMash (Central Scientific Research Institute of Machine Building), the leading institution of Roscosmos to support design, development and research into rocket and space articles, and M.V. Keldysh Research Center, the leading Russian entity for rocket engines.

International Launch Services (ILS) has formed a Failure Review Oversight Board (FROB) which will review the Commission’s final report and corrective action plan, in accordance with U.S. and Russian government export control regulations.  The FROB will begin in Moscow on January 30thand consists of ILS customers, industry subject experts, and insurance industry representatives. The FROB will provide an independent review of the investigation, root cause and corrective actions required prior to return to commercial flight.  After the conclusion of the FROB, the FROB report will be briefed to ILS customers and the launch insurance industry.

The anomaly occurred during the 4th and final burn of the Breeze M engine during a planned 9 hour and 15 minute mission. The 4th burn ended about four minutes early and the spacecraft was subsequently separated. The spacecraft, built by Thales Alenia Space for Russian satellite operator, Gazprom Space Systems, was successfully maneuvered to its orbital position and was declared fully operational on January 8th 2013 after completing its on orbit tests.

Additional information will be provided as it becomes available.
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Online Galactic Penguin SST

Hmmm....... again the long periods of operation by the Breeze-M seems to do no good to its reliability (or at least decreasing its margins) - someone put forward the hypothesis that the long 4+ hours coast between the third and fourth burns was almost entirely on the sunlit side of the Earth, which means that the fuel was not cooled down before the last burn, affecting their viscosity. Then when the burn took place, there was cavitation in the fuel lines, resulting in bearing destruction and fuel line leak. Does that make sense at all?  ???
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Offline anik

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someone put forward the hypothesis

It is not the hypothesis, it is an actual conclusion of commission.

Offline Stan Black

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While it was in flight I captured some additional events from
http://www.space-center.ru/LiveGroundTrack.aspx

582Конец АУ РН, отделение ОБ08.12.201213:23:25
662Начало поджатия08.12.201213:24:45
676Запуск МД08.12.201213:24:59
678Конец поджатия08.12.201213:25:01
955Выключение МД08.12.201213:29:38
965Конец 1-ого маневра08.12.201213:29:48
1020Начало разворота для ориентации по вектору скорости08.12.201213:30:43
1170Выход из зоны ИП08.12.201213:33:13
3410Конец разворота для ориентации по вектору скорости08.12.201214:10:33
3415Начало разворота для выполнения маневра08.12.201214:10:38
4015Начало поджатия08.12.201214:20:38
4015Конец разворота для выполнения маневра08.12.201214:20:38
4035Запуск МД08.12.201214:20:58
4037Конец поджатия08.12.201214:21:00
5129Выключение МД08.12.201214:39:12
7160Начало разворота для ориентации на Солнце08.12.201215:13:03
7460Конец разворота для ориентации на Солнце08.12.201215:18:03
10360Начало разворота для ориентации на Солнце08.12.201216:06:23
10660Конец разворота для ориентации на Солнце08.12.201216:11:23
11960Начало разворота для выполнения маневра08.12.201216:33:03
11984Открытие ТЗК08.12.201216:33:27
12560Начало поджатия08.12.201216:43:03
12584Запуск МД08.12.201216:43:27
12586Конец поджатия08.12.201216:43:29
13654Выключение МД08.12.201217:01:17
13654Выработка топлива из ДТБ08.12.201217:01:17
13729Начало поджатия08.12.201217:02:32
13735Сброс ДТБ08.12.201217:02:38
13737Конец поджатия08.12.201217:02:40
13865Вход в зону ИП08.12.201217:04:48
13900Начало разворота для ориентации на Солнце08.12.201217:05:23
14500Конец разворота для ориентации на Солнце08.12.201217:15:23
21152Начало разворота для ориентации на Солнце08.12.201219:06:15
21352Конец разворота для ориентации на Солнце08.12.201219:09:35
24578Начало разворота для ориентации на Солнце08.12.201220:03:21
24778Конец разворота для ориентации на Солнце08.12.201220:06:41
28004Начало разворота для ориентации на Солнце08.12.201221:00:27
28204Конец разворота для ориентации на Солнце08.12.201221:03:47
29717Начало разворота для ориентации на Солнце08.12.201221:29:00
29971Конец разворота для ориентации на Солнце08.12.201221:33:14
31430Начало разворота для выполнения маневра08.12.201221:57:33
31440Открытие ТЗК08.12.201221:57:43
32030Конец разворота для выполнения маневра08.12.201222:07:33
32030Начало поджатия08.12.201222:07:33
32040Запуск МД08.12.201222:07:43
32042Конец поджатия08.12.201222:07:45
32569Выключение МД08.12.201222:16:32
32579Конец 4-ого маневра08.12.201222:16:42
32690Начало разворота на отделение КА08.12.201222:18:33
33290Конец разворота на отделение КА08.12.201222:28:33
33290Начало зоны отделения КА08.12.201222:28:33
33300Отделение КА08.12.201222:28:43
41000Начало увода РБ09.12.201200:37:03
41015Окончание увода РБ09.12.201200:37:18
45130Начало увода РБ09.12.201201:45:53
45230Окончание увода РБ09.12.201201:47:33

Offline Chris Bergin

INTERNATIONAL LAUNCH SERVICES (ILS) FAILURE REVIEW OVERSIGHT BOARD (FROB) CONCLUDES THE YAMAL 402 PROTON LAUNCH ANOMALY INVESTIGATON

February 12, 2013- The ILS Failure Review Oversight Board (FROB) concluded its review on February 7, concurring on the most probable root cause and the associated corrective action plan of the December 8, 2012 anomaly of the Yamal 402 Proton launch The FROB analyzed the findings and recommendations of the Russian working group, which included participation from experts from TsNIIMash (Central Scientific Research Institute of Machine Building), M.V. Keldysh Research Center and Khrunichev State Research and Space Production Center (Khrunichev).

 

The members of the FROB agreed with the findings of the Russian investigation that the most probable root cause of the failure was due to a combination of adverse conditions which affected the operation of the Breeze M main engine during the startup of the 3rd burn causing damage to a bearing on the oxidizer side of the turbo pump. This ultimately resulted in the failure of the bearing during the 4th burn and caused the 4th burn of the Breeze M to end about four minutes early, with subsequent separation of the spacecraft. The spacecraft, built by Thales Alenia Space for Russian satellite operator, Gazprom Space Systems, was successfully maneuvered to its orbital position and was declared fully operational on January 8th 2013 after completing its on orbit tests.

 

“My sincere appreciation goes out to our customers, insurance underwriters and independent subject matter experts for their thorough and diligent participation in the ILS FROB process. We thank our customers for their support as ILS Proton proceeds towards return to flight,” said ILS Vice President of Programs and Operations, John Palmé.


The ILS Proton return to flight mission will be the Satmex 8 satellite for Satélites Mexicanos, S.A. de C.V. (Satmex) next month. Scheduling of this mission and of the remainder of the ILS Proton near term manifest for 2013 is currently being determined.

 

####

 

 

About ILS and Khrunichev

ILS is a leading launch services provider for global satellite operators and offers a complete array of services and support, from contract signing through mission management and on-orbit delivery.  ILS has exclusive rights to market the Proton vehicle to commercial satellite operators worldwide and is a U.S. company headquartered in Reston, VA., near Washington, D.C.  For more information, visit www.ilslaunch.com.

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Offline owais.usmani

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INTERNATIONAL LAUNCH SERVICES ISSUES ADDITIONAL DETAILS ON THE YAMAL 402 PROTON LAUNCH ANOMALY CAUSE AND CORRECTIVE ACTIONS


February 14, 2013 - International Launch Services (ILS) has issued additional details regarding the most probable root cause and corrective actions presented to the ILS Failure Review Oversight Board (FROB) concerning the Yamal 402 Proton launch anomaly which occurred on December 8, 2012.
 
The members of the FROB agreed with the findings of the Russian investigation that the most probable cause of the Yamal 402 Proton launch anomaly was due to a combination of adverse conditions which affected the operation of the Breeze M main engine during the startup of the 3rd burn.
The combination of adverse conditions were predominantly thermal in nature and affected the conditions at the oxidizer inlet line to the Breeze M main engine prior to the 3rd burn ignition and resulted in a large volume of oxidizer gas (rather than liquid oxidizer) at the engine inlet, exceeding the Breeze M main engine specifications. The volume of gas was ingested by the Breeze M turbopump at the start of the 3rd burn, leading to over-speed of the oxidizer turbopump bearing without the cooling normally supplied by liquid oxidizer. The over-speed damaged the bearing, which eventually led to the premature shutdown of the fourth burn. The adverse thermal conditions were due to higher than previously recorded propellant temperatures at liftoff combined with higher than previously recorded thermal soak-back of engine heat to the Breeze M prior to the 3rd burn.
Several corrective actions will be implemented, and include management of both satellite and Breeze M thermal requirements to ensure adequate margin to prevent future recurrence of this anomaly. No Breeze M hardware modifications are required.
The ILS Proton return to flight mission will be the Satmex 8 satellite for Satélites Mexicanos, S.A. de C.V. (Satmex) on March 27 (March 26 EST) from the Baikonur Cosmodrome in Kazakhstan. The corrective actions required by the FROB to prevent future recurrence of the anomaly have been started and are currently on schedule to support the new launch date. Scheduling of the remainder of the ILS Proton near term manifest for 2013 is currently being determined.

http://www.ilslaunch.com/newsroom/news-releases/international-launch-services-issues-additional-details-yamal-402-proton-laun

Offline edkyle99

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66 times Briz M has flown on Proton, and 18 more times as Briz K(M) on Rokot.  Amazing that new things keep happening.

 - Ed Kyle
« Last Edit: 02/14/2013 08:01 pm by edkyle99 »

Offline Stan Black

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Quote
December 8 – Yamal-402 – Proton-M/Briz-M – Baikonur 200/39

Briz-M upper stage for this mission was today delivered to Baykonur
http://www.khrunichev.ru/main.php?id=1&nid=2637 (in Russian)

According to Rui this launch was to use 99528
http://www.zenite.nu/orbita/index.php?catid=4

Briz-M 99528 was previously delivered for Sirius-FM6
http://www.khrunichev.ru/main.php?id=1&nid=2295

99528 was then to be used for Intelsat-23

This was the eighth delivery of Briz-M for 2012
http://www.aex.ru/news/2012/11/1/99554/

So were the two previously delivered Briz-M for Sirius-FM6 and Luch-5B with Yamal-300K ever returned to Moscow for refurbishment?
http://forum.nasaspaceflight.com/index.php?topic=27791.msg952783#msg952783
Or were they repaired on site at Baikonur?



http://www.gazprom-spacesystems.ru/ru/news/publications/index.php?ELEMENT_ID=2142
Quote
«Новости космонавтики»
01.2013
А. Красильников
После этого Роскосмос принял решение детально перепроверить произведенные «Бризы-М»: №99528 и №99533, находившиеся на космодроме, а также №99534 и №99535, пребывавшие в Центре Хруничева. На это потребовалось время. В результате 14 октября на «Протоне-М» первым после аварии полетел спутник Intelsat 23. Причем для его запуска использовался «Бриз-М» №99534, доставленный на Байконур 21 сентября, а не №99528, хранившийся в МИКе площадки 92А. А вот «Луч-5Б» и «Ямал-300К», как изначально планировалось, отправились на орбиту на блоке №99533.
Как сообщил НК заместитель директора Завода по эксплуатации ракетно-космической техники Центра Хруничева по летно-испытательной базе «Байконур» Леонид Горюшкин, «Бризы-М» №99528 и №99533 были подвергнуты специальной проверке прямо в МИКе площадки 92А.

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