Do you know how to translate "построитель местной вертикали"?
It's a device which finds Earth surface normal vector (by detecting Earth limb in a few directions).
Thanks gospacex.
Do you know how this device is called in technical English ?
translate.google.com works pretty well to give you the general gist of something. Better that Babelfish ever was (works for more languages, too! Including Latin.).
Do you know how to translate "построитель местной вертикали"?
It's a device which finds Earth surface normal vector (by detecting Earth limb in a few directions).
Thanks gospacex.
Do you know how this device is called in technical English ?
horizon detector
I've also seen "horizon sensor".
The little airlock module (pictured) launched together with MRM-1 will eventually be berthed to the lateral docking port of MLM, currently configured to be hybrid passive. This implies that the airlock module docking adapter will be hybrid active. However, I can't find a photo showing an active hybrid adapter on the airlock module, and I have not yet seen a photo of the docking side of the airlock module at ISS to date. The lower photo attached is from Energia, and it looks like the airlock module docking adapter has a hybrid collar, but no docking system is pictured.
So, what kind of docking adapter is mounted on the airlock module?
Or, let me ask the question a different way: if a hybrid/APAS collar is used, can a vehicle be berthed without an active docking adapter? Could it simply be pushed against the collar of the passive vehicle, and then the latches in the collars could engage?
If this is the case, and the CDA does use the hybrid/APAS collar, then, in theory, the little airlock may be used *someday* on the US segment.
In NK n°127, in the article about the Soyuz failure of 14th may 1996, it is written :
“Комета” на Байконуре не была подорвана системой АПО, которая была незадействована, дабы избежать аварии, происшедшей при одном из последних запусков КА данного типа, когда прошла команда на подрыв аппарата вместо команды на отделение третьей ступени.
I don't find any mention of such an incident in the Kometa launch archives. Someone can help ?
In NK n°127, in the article about the Soyuz failure of 14th may 1996, it is written :
“Комета” на Байконуре не была подорвана системой АПО, которая была незадействована, дабы избежать аварии, происшедшей при одном из последних запусков КА данного типа, когда прошла команда на подрыв аппарата вместо команды на отделение третьей ступени.
I don't find any mention of such an incident in the Kometa launch archives. Someone can help ?
If I understand this…
The APO is an explosive charge designed to destroy a satellite. Kosmos 2243 failed when it’s APO triggered at orbit insertion; and the remains decayed uncontrolled after nine days.
The Kometa launch in 1996 was one of two launches that year where the payload fairing came apart. In the case of the Kometa the fairing failed at 49 seconds, the satellite broke apart, but the rocket kept going. After 121 seconds it deviated from the flight path and aborted by 124 seconds. Because of the previous accident this Kometa’s APO was not triggered.
The second launch failure in 1996 was also at 49 seconds. It did not involve a Kometa and the satellite did blow itself up with the APO.
http://www.novosti-kosmonavtiki.ru/content/numbers/046/04.shtmlhttp://www.novosti-kosmonavtiki.ru/content/numbers/082/16.shtmlhttp://www.novosti-kosmonavtiki.ru/content/numbers/125/06.shtmlhttp://www.novosti-kosmonavtiki.ru/content/numbers/127/07.shtmlThe two failures listed in 1996 (May 14 and June 20) were due to a manufacturing defect with the fairing release mechanism. Since the fairings for the two flights were manufactured in a batch, the same defect was repeated on both fairings. The cause was identified, other fairings in the batch were repaired, and corrective actions were taken to ensure that this defect was not repeated. These failures were the only two in 195 Soyuz family launches, going back to 1990. Since these failures, Soyuz family LVs have been launched sucessfully 58 consecutive times through December 31, 2000.
The proposed Hub module for ISS has a 3.3 meter diameter, the first time I have seen a module from Energia with this diameter. Has anyone seen an earlier proposal from Energia with a 3300 mm diameter module?
Maybe not the right place to post it, but I'd like to share a good video of a Soyuz showing the start of the SKDU. It was probably shot from Salyut-6.
I've extracted this video from a very good German documentary on Intercosmos program. I don't know why, but when I've made the extraction, the size changed. So you have to read it in VLC and choose "16:9" to watch it normally.
http://doc.gostorgi.ru/7/2010-04-08/740237/1.DOC Item № 1 production and the delivery of fairings for the launch of KGU 44S, 46S, K1 - 14S737-0000-OTU. Fairing: for the launch of KGU 44S quantity 1 - HF 13991, Mirny, Arkhangelsk Oblast; for the launch of KGU 46S quantity 1 - HF 13991, Mirny, Arkhangelsk Oblast; for the launch of KGU K1 quantity 1 - HF 13991, Mirny, Arkhangelsk Oblast. Item № 2 production and the delivery of two fairings, one for the launch of KGU 45K and a second held in reserve - 813BK-0100-OTU. Fairing: for the launch of KGU blok 45K, quantity 1 - HF 11284, Tyura-Tam, republic Kazakhstan.Lavochkin awarded contract for three fairings for KGU 44S, 46S and K1.
http://www.rosspending.ru/fk/contract/0018710005071/14F113 Uragan-M 724-746
Planned date for conclusion of contract: 12.2011
http://www.rosspending.ru/fk/contract/0025907000269/?year=2006 So five Uragan-M remaining to be delivered by the end of 2011. Two solo launches from Plesetsk; 14S737 is the fairing also used for 14F112 Meridian. The latest launch of GLONASS in December was blok 43 with satellites 739, 740 and 741.
14F113 Uragan-M 747-749
Planned date for conclusion of contract: 12.2012
http://www.rosspending.ru/fk/contract/0025910000148/?year=201014F113 Uragan-M 736-746
http://www.spels.ru/index.php?option=com_docman&task=doc_download&gid=374&Itemid=34 The inspection and additional certification tests of electrical radio components of foreign production. Blok 41 and 40 with 730 to 735 were the delayed launches with the Uragan-M requiring modifications.
14F113 Uragan-M 715-720
http://www.rosspending.ru/fk/contract/0025907000237/?year=200414F113 Uragan-M 721-723
http://www.rosspending.ru/fk/contract/0025907000261/?year=2005
I'm searching for the radio recording of the Yuri Levitan annoncement of Gagarin launch. Any help?