Angara-1.2PP first launch - July 9, 2014

[ostangen]

Perhaps NOTAMs for ANGARA launch?

V5340/14 - TEMPO DANGER AREA ACT WI COORD: 6935N 05318E-6913N 05311E-6851N 05214E-6848N 05114E- 6910N 05119E-6932N 05216E-6935N 05318E. SFC - UNL, 25 0600-0830 1200-2030, 26-28 1100-1630, 25 JUN 06:00 2014 UNTIL 28 JUN 16:30 2014. CREATED: 21 JUN 09:30 2014

V5339/14 - ATS RTE SEGMENTS CLSD: B954 RINOV - ABGAR, G108 LUKEN - OLODA. SFC - UNL, 25 0600-0830 1200-2030, 26-28 1100-1630, 25 JUN 06:00 2014 UNTIL 28 JUN 16:30 2014. CREATED: 21 JUN 08:23 2014

P4172/14 - TEMPO DANGER AREA ACT WI COORD: 5843N 16024E-5823N 16106E-5724N 16205E-5653N 16207E- 5714N 16126E-5813N 16030E-5843N 16024E. SFC - UNL, 25 0600-0830 1200-2030, 26-28 1100-1630, 25 JUN 06:00 2014 UNTIL 28 JUN 16:30 2014. CREATED: 21 JUN 09:43 2014

P4171/14 - ATS RTE B240 SEGMENT TILICHIKI NDB (TK) - OKLED CLSD. SFC - UNL, 25 0600-0830 1200-2030, 26-28 1100-1630, 25 JUN 06:00 2014 UNTIL 28 JUN 16:30 2014. CREATED: 21 JUN 08:43 2014

[input~2]

Perhaps NOTAMs for ANGARA launch?

Doesn't look like it to me, but here is a visualization of these 2 zones

[anik]

Doesn't look like it to me

This is it.

[baldusi]

Perhaps NOTAMs for ANGARA launch?

Doesn't look like it to me, but here is a visualization of these 2 zones

This is a sub orbital flight after all. Isn't this the up drop zone of the upper stage the Kura Test Range?

[Galactic Penguin SST]

Any rumored launch time floating around more precise than the air space closure time?

[Artyom.]

On the pad  !

Source

[Artyom.]

And confirmation from the Russian TV channel - http://www.tvc.ru/news/show/id/43149.

[JBF]

On the pad  !

Source

Wow that is a massive MST.

[edkyle99]

On the pad  !

Source

Wow that is a massive MST.

It is designed to also support the big Angara 5 version.

 - Ed Kyle

[Galactic Penguin SST]

Information about this flight: http://www.tsenki.com/launch_services/help_information/launch/2014/?EID=111219

Someone please remind me what kind of changes were made to the RD-0124 engine on the Soyuz-2 to form the RD-0124A engine on the Angara...... 

[asmi]

Someone please remind me what kind of changes were made to the RD-0124 engine on the Soyuz-2 to form the RD-0124A engine on the Angara...... 

As far as I remember it was certified for longer burn time. There appears to be no changes in hardware, as that engine was once successfully test-fired for 3000 seconds.

[Artyom.]

More photos 

_{P.S. Unofficially: launch time - 11:15 UTC or 14:15}

[Artyom.]

And we have video - http://tvzvezda.ru/news/vstrane_i_mire/content/201406260842-rnpb.htm 

[Galactic Penguin SST]

Someone reported a launch time of 14:15 UTC. 

[Phillip Clark]

I have just realised that this launch will be the first time that there has been a single-chamber engine on a Russian/Soviet liquid-propellant launch vehicle.   (Pause - what about those launched from submarines?)

[JBF]

I have just realised that this launch will be the first time that there has been a single-chamber engine on a Russian/Soviet liquid-propellant launch vehicle.   (Pause - what about those launched from submarines?)

If I remember correctly most Russian/USSR missiles were 4 chamber.

[asmi]

I have just realised that this launch will be the first time that there has been a single-chamber engine on a Russian/Soviet liquid-propellant launch vehicle.   (Pause - what about those launched from submarines?)

Hmmm - what about Soyuz-2.1v (NK-33-1)? Or Zenit (second stage's RD-120)?
Proton engines are single-chamber too - just that there are several of them burning at the same time.

[Skyrocket]

I have just realised that this launch will be the first time that there has been a single-chamber engine on a Russian/Soviet liquid-propellant launch vehicle.   (Pause - what about those launched from submarines?)

Hmmm - what about Soyuz-2.1v (NK-33-1)? Or Zenit (second stage's RD-120)?
Proton engines are single-chamber too - just that there are several of them burning at the same time.

Soyuz-2.1v has the additional RD-0110R four-chambered stearing engine (http://www.kosmonavtika.com/lanceurs/soyouz/version/14A15/14A15.html)
and the Zenit second stage has the  additional RD-8 four-chambered stearing engine (http://www.russianspaceweb.com/zenit_stage2.html)

The liquid fueled SLBMs (R-27 and R-29 versions) have also stearing engines.

[asmi]

Soyuz-2.1v has the additional RD-0110R four-chambered stearing engine (http://www.kosmonavtika.com/lanceurs/soyouz/version/14A15/14A15.html)
and the Zenit second stage has the  additional RD-8 four-chambered stearing engine (http://www.russianspaceweb.com/zenit_stage2.html)

The liquid fueled SLBMs have also stearing engines.

But that doesn't make single-chamber main engine any less single-chamber
Anyways, this is OT here.

[Prober]

The guy with the Gun was a little disturbing; but that's Russia.