Last time it leaps into space, I called it the Silver Hypergolic Monster(TM) - and failed right before the finish line. But that was three months ago, and the monster has seen quite a bit of injuries and bruises since its birth in the mid-1960s, and there's not much doubt that it can rise again, or at least within those that operates these creatures.
And right just in time too - this launch is carrying a much needed satellite for a Mexican satellite communication operator. Satmex-8 is replacing a 15 year old satellite that is reported to be running out of fuel only two months from now! With 4 failures in just 2 years and 22 launches, this really is the make or break moment - another miss and the Proton operators are risking another exodus of customers. So as with the Dragon, let's see what happens today.... :shifty:
This is the 1st commercial mission of the year for ILS and the 78th ILS Proton mission since the Proton April 1996 first commercial flight.
This is the 1st SATMEX satellite launched with Proton and the 25th Space Systems/Loral-built satellite launched on Proton.
Launch location:
Baikonur Launch pad no. 200/39 46° 2'23.85"N, 63° 1'54.98"E
Launch dates and times:
[table="head"]{colsp=6}Launch times
Time Zone|
Baikonur / UTC+6
|
Moscow / UTC+4
|
Universal / UTC
|
Washington / EDT
|
Los Angeles / PDT
Launch time (Primary):
|
01:06:48
|
23:06:48
|
19:06:48
|
15:06:48
|
12:06:48
on:
|
Mar. 27, 2013
|
Mar. 26, 2013
|
Mar. 26, 2013
|
Mar. 26, 2013
|
Mar. 26, 2013
{colsp=6}
[highlight][eventTimer]2013-03-26 19:06:48?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Satmex-8 Launch[/highlight]
[/table]
Live Coverage Of The Launch:
PAYLOAD
Satmex-8 communication satellite:
Mission Summary
Space Systems/Loral (SS/L) announced in May 2010 that it has been selected to provide a satellite for Satélites Mexicanos, S.A. de C.V. Satmex 8 is a high-power C and Ku-band satellite that replaces Satmex 5 and will provide Fixed Satellite Services (FSS) in both North and South America.
The new satellite will augment the current Satmex fleet in providing services such as broadband, voice and data transmission, and video broadcasting. Satmex 8 is a 24 C and 40 Ku-band transponders satellite and it is being designed to be located at 114.9 degrees West. Satmex 8 is based on SS/L’s high power LS-1300 spacecraft bus which provides the flexibility for a broad range of applications. It has a planned mission life of 15 years.
[table="head"]{colsp=2}Summary
Parameter|
Value
Working Orbit:
|
GEO
Orbital Location:
|
116.8° West
Coverage:
|
USA, Central/South America
ApA at separation:
|
35786 km
PeA at separation:
|
6159 km
Inc at separation:
|
18.38°
[/table]
[table="head"]Characteristics|
Satmex-8
Customer:
|
Prime contractor:
|
Platform:
|
Mass at Separation:
|
Dry Mass:
|
Stabilization:
|
Dimensions (stowed):
|
Batteries:
|
Payload:
|
- 24 C-band transponders
- 40 Ku-band transponders
Life time:
|
Coverage:
|
|
[/table]
Launch Vehicle:
[table="head"]{colsp=2}Characteristics
|[table="head"]{colsp=2}
Proton-M / Briz-M
Prime contractor:
|
GRAU Index:
|
Height:
| 58.2 m with upper stage and payload fairing
Diameter:
| max 7.4 m
Liftoff mass:
| 705 metric tonnes
Payload mass:
| ~22 tonnes at LEO
1st stage:
|
- 6 X RD-275 engines
- Empty 30.6 tonnes
- Propellants 419.41 tonnes (UDMH and NTO)
- Thrust in vacuum 1069.8 tonnes of force
- Thrust at sea level 971.4 tonnes of force
2nd stage:
|
- 1 X RD-0211 engine 3 X RD-0210 engines
- Empty 11.4 tonnes
- Propellants 156.113 tonnes (UDMH and NTO)
- Thrust in vacuum 237.4 tonnes of force
3rd stage:
|
- 1 X RD-0213 engine & 1 X RD-0214 vernier engine
- Empty 3.7 tonnes
- Propellants 46.562 tonnes (UDMH and NTO)
- Thrust in vacuum 59.36 (core) + 3.15 (vernier) tonnes of force
Upper Stage:
|
- GRAU Index: 14S43
- Common Name: Briz-M
- Designer & Manufacturer: Khrunichev Space Centre
- Dimensions: Length 2.654 m, Diameter 4 m
- Empty Mass 2.2 tonnes
- Propellants 6 660 kg UDMH + 13 260 kg N2O4
- Flight time: no less than 24 hours
- Main Engine: 1 X 14D30
- Thrust in vacuum 2.0 tonnes of force
- ISP 328.6 s
- Main engine restarts: up to 8 times
- Precision Manoeuvering Engines: 4 X 11D458
- Thrust in vacuum 400 N each
- ISP 252 s
- RCS Engines: 12 X 17D58E
- Thrust in vacuum 13.3 N each
- ISP 274 s
Payload Fairing:
|
- Diameter 4.35 m
- Length 11.6 m
[/table]
[/table]
The vehicle's
reliability statistics according to
http://www.spacelaunchreport.com/log2012.html#rate:
Code:
================================================================
Vehicle Successes/Tries Realzd Pred Consc. Last Dates
Rate Rate* Succes Fail
================================================================
Proton-M/Briz-M 56 62 .90 .89 0 12/08/12 2001-
Satmex-8 Ascent Profile
The Proton-M first three stages place the orbital unit (OU), which consists of a Breeze-M upper stage, adapter system and Satmex-8, into a 51.5° inclination suborbital trajectory.
Proton-M powered flight lasts 582 seconds. The OU powered flight begins at the moment of the third stage separation.
Immediately after the separation of the third stage booster, the Breeze-M stability engines start, damping the angular velocities of the third stage separation and then providing orbital unit orientation and stability during coast flight along a suborbital trajectory to await the first burn. The upper stage follows a four-burn injection profile.
Satmex-8 Ascent Timeline
[TABLE="head"]Event|Time rel lift-off|Time UTC|Comment
Ignition Start Sequence|-00:00:02.5|19:06:45.5|
Stage 1 Ignition (40% thrust)|-00:00:01.75|19:06:46.25|
Command Stage 1 (100% thrust)|-00:00:00.9|19:06:47.1|
Maximum Dynamic Pressure|00:01:02|19:07:50|
1st/2nd Stage Separation|00:02:00|19:08:48|
2nd/3rd Stage Separation|00:05:27|19:12:15|
Payload Fairing Separation|00:05:47|19:12:35|
3rd Stage/Breeze M Separation|00:09:42|19:16:30|
1st Burn Ignition|00:11:46|19:18:34|
1st Burn Shutdown|00:16:13|19:23:01|1st Burn's Duration 00:04:27
2nd Burn Ignition|01:07:33|20:14:21|
2nd Burn Shutdown|01:25:19|20:32:07|2nd Burn's Duration 00:17:46
3rd Burn Ignition|03:28:30|22:35:18|
3rd Burn Shutdown|03:41:29|22:48:17|3rd Burn's Duration 00:12:59
APT Jettison|03:42:19|22:49:07|
4th Burn Ignition|03:43:46|22:50:34|
4th Burn Shutdown|03:48:17|22:55:05|4th Burn's Duration 00:04:31
5th Burn Ignition|08:51:35|03:58:23|
5th Burn Shutdown|08:59:06|04:05:54|5th Burn's Duration 00:07:31
Spacecraft Separation|09:13:00|04:19:48|
[/TABLE]
Weather forecast for Baikonur, Kazakhstan on March 27, 2013 (1 a.m.)
Partly cloudy in the evening, then clear. Low of 3C. Breezy. Winds from the South at 10 to 20 km/h.
Time|Temps|Dew Point|Relative Humidity|Precip|Snow|Cloud cover|Pressure|Wind|Weather
2 AM|8°C|-7°C|33%|0%|0%|0%|1020 hPa|18 km/h S|
Clear
References
http://www.federalspace.ru
http://tvroscosmos.ru
http://www.khrunichev.ru
http://www.ilslaunch.com
http://tihiy.fromru.com/Rn/RN_Proton.htm
http://space.skyrocket.de/doc_sdat/satmex-8.htm
www.satmex.com
http://ssloral.com/html/pressreleases/pr20121129.html
http://www.tsenki.com
http://forum.nasaspaceflight.com
http://www.novosti-kosmonavtiki.ru
http://www.spacelaunchreport.com
http://english.wunderground.com/cgi-bin/findweather/getForecast?query=44.84999847,65.50000000