Quote from: smoliarm on 02/01/2013 11:39 amDoes [winds: 6 knots & seas: 6.5’] qualify as “rough sea” ??6 knots translates into 3.1 m/sec – it’s almost nothing, as I understand – am I right?seas: 6.5’ – 2 meter waves; can they make an ocean oil rig “unstable” ??As a 20 year US Navy vet, I will state unequivocably that 6 knot winds and 6.5ft seas are nothing to a vessel the size of the Odyssey platform, particularly when it is ballasted down for launch. In addition, such platforms usually have some form of active stabilisation.
Does [winds: 6 knots & seas: 6.5’] qualify as “rough sea” ??6 knots translates into 3.1 m/sec – it’s almost nothing, as I understand – am I right?seas: 6.5’ – 2 meter waves; can they make an ocean oil rig “unstable” ??
Quote from: Proponent on 02/01/2013 03:03 pmDo we know whether Zenit actually has hold-down following ignition? I thought the usual Russian practice was to ignite at a low thrust level without hold-down, have a quick look to see whether things are OK, and then throttle up and go.Observe pyros firing right at start of video.
Do we know whether Zenit actually has hold-down following ignition? I thought the usual Russian practice was to ignite at a low thrust level without hold-down, have a quick look to see whether things are OK, and then throttle up and go.
Yeah, for the quality of the stream (not at all great), the initial ascent didn't strike me as odd.
http://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.
likely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.
Quote from: owais.usmani on 02/01/2013 10:29 amhttp://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.got a feeling they are on to the problem. Its the same Phobos Grunt again. My question would be: Will Russia double down and quickly launch again or run away from Sea Launch?
Quote from: Prober on 02/01/2013 05:52 pmQuote from: owais.usmani on 02/01/2013 10:29 amhttp://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.got a feeling they are on to the problem. Its the same Phobos Grunt again. My question would be: Will Russia double down and quickly launch again or run away from Sea Launch?How is this related to Phobos Grunt? That Zenit launched just fine.
Quote from: Lars_J on 02/01/2013 05:54 pmQuote from: Prober on 02/01/2013 05:52 pmQuote from: owais.usmani on 02/01/2013 10:29 amhttp://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.got a feeling they are on to the problem. Its the same Phobos Grunt again. My question would be: Will Russia double down and quickly launch again or run away from Sea Launch?How is this related to Phobos Grunt? That Zenit launched just fine.loss of control.....remember PG used a brand new controller.
Quote from: Prober on 02/01/2013 06:05 pmQuote from: Lars_J on 02/01/2013 05:54 pmQuote from: Prober on 02/01/2013 05:52 pmQuote from: owais.usmani on 02/01/2013 10:29 amhttp://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.got a feeling they are on to the problem. Its the same Phobos Grunt again. My question would be: Will Russia double down and quickly launch again or run away from Sea Launch?How is this related to Phobos Grunt? That Zenit launched just fine.loss of control.....remember PG used a brand new controller.But that was a different controller... Phobos-Grunt had some jury-rigged custom solution. Separate from the Zenit LV.
A quick analysis of telemetry data received leads to a preliminary conclusion that the first-stage propulsion system and control system of the launch vehicle were operating normally.
Document review conducted during this day at the factory power plant (NGO "Energomash") and management systems (SPC AP) showed that there were no abnormalities in their production.
What does this have to do with Russia? It's an Ukrainian rocket?
said that no disturbance of the ocean during the launch was not. If it were, it would have moved the start (to another date)," - said the source.
Quote from: Lars_J on 02/01/2013 06:16 pmQuote from: Prober on 02/01/2013 06:05 pmQuote from: Lars_J on 02/01/2013 05:54 pmQuote from: Prober on 02/01/2013 05:52 pmQuote from: owais.usmani on 02/01/2013 10:29 amhttp://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.got a feeling they are on to the problem. Its the same Phobos Grunt again. My question would be: Will Russia double down and quickly launch again or run away from Sea Launch?How is this related to Phobos Grunt? That Zenit launched just fine.loss of control.....remember PG used a brand new controller.But that was a different controller... Phobos-Grunt had some jury-rigged custom solution. Separate from the Zenit LV.but suffered loss of control
Quote from: Prober on 02/01/2013 05:52 pmQuote from: owais.usmani on 02/01/2013 10:29 amhttp://ria.ru/science/20130201/920839804.htmlQuotelikely to have been due to a failure in the control system, according to RIA Novosti source in the space industry.got a feeling they are on to the problem. Its the same Phobos Grunt again. My question would be: Will Russia double down and quickly launch again or run away from Sea Launch?What does this have to do with Russia? It's an Ukrainian rocket?
Quote from: anik on 02/01/2013 01:14 pmI was told that there was not 100% thrust of engine at rocket liftoff.If that's the case, it's a really "nice" feature - to have the vehicle issue a launch commit command even though its propulsion system didn't satisfy nominal operation criteria. I find that a little hard to believe.
I was told that there was not 100% thrust of engine at rocket liftoff.