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Arianespace’s no. 2 Soyuz mission from French Guiana has been given the launch go-ahead, moving preparations into their final phase for a nighttime liftoff tomorrow with six satellite passengers.
For its second Soyuz launch from the Guiana Space Center in French Guiana, Arianespace will orbit the Pleiades satellite for French space agency CNES, along with four ELISA demonstrator satellites and the Chilean Earth observation satellite, SSOT.
Launch location:
Kourou ELS 5°18'18"N 52°50'02"W
Launch dates and times:
[table="head"]{colsp=7}Launch times (updated)
Time Zone|Australia - Sydney/AEST|Moscow / MSK/ UTC+4|CET UTC+1|Universal / UTC|Washington / EST|French Guiana
Launch time:|1:03:08 pm|06:03:08|03:03:08 am|02:03:08|9:03:08 pm|11:03:08 pm
on:|Dec. 17, 2011|Dec. 17, 2011|Dec. 17, 2011|Dec. 17, 2011|Dec. 16, 2011|Dec. 16, 2011
{colsp=7}[highlight][eventTimer]2011-12-17 2:03:08?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Joint Pleiades, ELISA, SSOT Launch[/highlight][/table]
Live Coverage
PAYLOAD 1
Pleiades 1 Earth observation satellite
Pleiades 1 is the first of two dual-use, very-high-resolution satellites in the Pleiades Earth observation system. Both are built by Astrium Satellites in Toulouse for French space agency CNES. The first satellite will be joined by its twin brother Pleiades 2 within a year.
[table="head"]Characteristics|Values
Orbit|sun-synchronous, 695 km altitude
Weight at launch|970 kg
Electrical power|1,500 W
Design life|5 years
[/table]
Two Pleiades satellites are supposed to work together with SPOT-5 optical observation satellite.
The SPOT-5 optical Earth observation satellite combines the advantages of a relatively wide imaging swath and sub-3-metre resolution. Today, new and evolving civil and military challenges facing Europe call for different levels of image resolution.
The Pleiades optical satellites will provide imagery covering a smaller area but with a resolution of 0.70 m.
Together, SPOT and Pleiades will offer a broader range of complementary data better able to meet the diverse requirements of civil users—for example, cartographers, volcanologists, geophysicists, hydrologists and urban planners—and military users.
The Pleiades optical system is being developed under CNES supervision as part of a joint effort with Italy, alongside the Cosmo-Skymed radar imaging system that is under the responsibility of the Italian space agency (ASI).
This French-Italian cooperation will bring users a richer variety of large and small-area optical and radar imagery than ever before, at high and low resolutions.
PAYLOAD 2
4 * ELISA demonstrators satellites
ELISA - The four ELISA demonstrator satellites, part of a joint program between French defense procurement agency DGA and space agency CNES, were produced by a partnership between Astrium Satellites and Thales Airborne Systems.
[table="head"]Characteristics|Values
Orbit: sun-synchronous|700 km altitude
Weight at launch|120 kg each
Platform|Myriade, designed by CNES
Design life|over 3 years
[/table]
The ELISA project will be used to map radar transmitters across the planet, and determine their characteristics.
http://www.defense.gouv.fr/dga/actu...au-domaine-du-renseignement-spatial-militaire
SSOT Earth observation satellite
SSOT - "Sistema Satelital para la Observacion de la Tierra" is an Earth observation satellite built by Astrium Satellites for Chilean armed forces.
[table="head"]Characteristics|Values
Orbit: sun-synchronous|610 km altitude
Weight at launch|117 kg
Platform|Myriade, designed by CNES
Design life|5 years
[/table]
Sistema Satelital para Observacion de la Tierra (SSOT) is an high resolution, space-based Earth Observation System ordered by the Chilean Ministry of Defense (MoD). The Chilean MoD and EADS Astrium signed a contract covering development of the system on August 7, 2008.
In addition to the spacecraft, the SSOT also includes a ground control segment and image processing facilities to be located in Chile.
The SSOT is equipped with a latest-generation payload capable of supplying images with a resolution of 1.45 meters in panchromatic mode and 5.8 meters in each of four color bands in multispectral mode. It is intended to serve both military and civil customers using high quality images for applications such as cartography; agricultural management; forestry; water, mineral and oil resources; crop protection; natural disaster response; and urban planning.
Launch Vehicle:
[table="head"]{colsp=2}Characteristics
|[table="head"]{colsp=2}
[/table]
[/table]
The launch vehicle's reliability standings
According to http://www.spacelaunchreport.com/log2011.html#rate:
Ascent profile
Weather Forecast for Sinnamary, French Guiana on December 17, 2011 (11 p.m.)
Time|Temps|Wind Chill|Heat Index|UV Index|Dew Point|Relative Humidity|Precip|Snow|Clouds|Visibility|Wind|Weather
11 PM|24°C|24°C|24°|0 Low|23°C|93%|40%|0%|44%|16KM|NNE 1mph|
Sct T-Storms
References
http://www.esa.int
http://www.cnes.fr
http://www.arianespace.com
http://forum.nasaspaceflight.com
http://www.novosti-kosmonavtiki.ru
http://astronautique.actifforum.com
http://www.spacelaunchreport.com
http://www.cnes.fr/web/CNES-en/3236-pleiades.php
http://www.defense.gouv.fr/dga/actu...au-domaine-du-renseignement-spatial-militaire
http://www.samspace.ru
http://www.laspace.ru
http://www.intellicast.com
http://www.good-stuff.co.uk/suntimes/sunmap.php
For its second Soyuz launch from the Guiana Space Center in French Guiana, Arianespace will orbit the Pleiades satellite for French space agency CNES, along with four ELISA demonstrator satellites and the Chilean Earth observation satellite, SSOT.
Launch location:
Kourou ELS 5°18'18"N 52°50'02"W
Launch dates and times:
[table="head"]{colsp=7}Launch times (updated)
Time Zone|Australia - Sydney/AEST|Moscow / MSK/ UTC+4|CET UTC+1|Universal / UTC|Washington / EST|French Guiana
Launch time:|1:03:08 pm|06:03:08|03:03:08 am|02:03:08|9:03:08 pm|11:03:08 pm
on:|Dec. 17, 2011|Dec. 17, 2011|Dec. 17, 2011|Dec. 17, 2011|Dec. 16, 2011|Dec. 16, 2011
{colsp=7}[highlight][eventTimer]2011-12-17 2:03:08?before|after;%dd% Days %hh% Hours %mm% Minutes %ss% Seconds %c%[/eventTimer] Joint Pleiades, ELISA, SSOT Launch[/highlight][/table]
Live Coverage
- http://www.arianespace.tv/ - begins 20 minutes before the launch
- http://tsenki.com/broadcast/ - three stand-ups: 3:00-3:45 MSK, 5:25-7:30 MSK (launch is at 6:03), 9:10-10:10 MSK
- http://www.vesti.ru/videos?vid=onair
PAYLOAD 1
Pleiades 1 Earth observation satellite
Pleiades 1 is the first of two dual-use, very-high-resolution satellites in the Pleiades Earth observation system. Both are built by Astrium Satellites in Toulouse for French space agency CNES. The first satellite will be joined by its twin brother Pleiades 2 within a year.
[table="head"]Characteristics|Values
Orbit|sun-synchronous, 695 km altitude
Weight at launch|970 kg
Electrical power|1,500 W
Design life|5 years
[/table]
Two Pleiades satellites are supposed to work together with SPOT-5 optical observation satellite.
The SPOT-5 optical Earth observation satellite combines the advantages of a relatively wide imaging swath and sub-3-metre resolution. Today, new and evolving civil and military challenges facing Europe call for different levels of image resolution.
The Pleiades optical satellites will provide imagery covering a smaller area but with a resolution of 0.70 m.
Together, SPOT and Pleiades will offer a broader range of complementary data better able to meet the diverse requirements of civil users—for example, cartographers, volcanologists, geophysicists, hydrologists and urban planners—and military users.
The Pleiades optical system is being developed under CNES supervision as part of a joint effort with Italy, alongside the Cosmo-Skymed radar imaging system that is under the responsibility of the Italian space agency (ASI).
This French-Italian cooperation will bring users a richer variety of large and small-area optical and radar imagery than ever before, at high and low resolutions.
PAYLOAD 2
4 * ELISA demonstrators satellites
ELISA - The four ELISA demonstrator satellites, part of a joint program between French defense procurement agency DGA and space agency CNES, were produced by a partnership between Astrium Satellites and Thales Airborne Systems.
[table="head"]Characteristics|Values
Orbit: sun-synchronous|700 km altitude
Weight at launch|120 kg each
Platform|Myriade, designed by CNES
Design life|over 3 years
[/table]
The ELISA project will be used to map radar transmitters across the planet, and determine their characteristics.
http://www.defense.gouv.fr/dga/actu...au-domaine-du-renseignement-spatial-militaire
PAYLOAD 3Elisa est un demonstrateur technologique lance par la Direction generale de l’armement (DGA) et constitue de quatre satellites volant en formation a 700 km d’altitude. Il vise a demontrer la capacite a localiser et caracteriser des radars au sol depuis l’Espace. Pendant au moins 3 ans, les equipes de la DGA installees a Bruz (pres de Rennes) en collaboration avec les forces armees, notamment la Direction du renseignement militaire (DRM) de Creil, vont explorer les moyens d’ameliorer la precision et la qualite des informations recueillies. Le projet Elisa s’inscrit dans la logique engagee il y a 15 ans avec les satellites Cerises et Clementine poursuivie a partir de 2004 avec le demonstrateur Essaim qui a permis d’experimenter le recueil de renseignements electromagnetiques dans le domaine des telecommunications.
L’ensemble des enseignements tires de ces demonstrateurs vise a preparer le programme CERES dont la mise en orbite est prevue d’ici la fin de la decennie. Ce programme permettra de localiser et identifier des signaux emis par les systemes adverses notamment pour cartographier les centres de telecommunications et les radars dans les zones de crise, et pour evaluer leur niveau d’activite. Ainsi CERES permettra par exemple de preciser le danger que representent les radars ennemis afin de garantir la suprematie des avions francais, ou encore de determiner l’architecture des reseaux de communication adverses. CERES contribuera directement a la fonction « connaissance et anticipation » du Livre blanc sur la defense et la securite nationale.
La DGA a confie a Astrium et Thales Systemes Aeroportes la realisation des quatre satellites et du segment sol.
SSOT Earth observation satellite
SSOT - "Sistema Satelital para la Observacion de la Tierra" is an Earth observation satellite built by Astrium Satellites for Chilean armed forces.
[table="head"]Characteristics|Values
Orbit: sun-synchronous|610 km altitude
Weight at launch|117 kg
Platform|Myriade, designed by CNES
Design life|5 years
[/table]
Sistema Satelital para Observacion de la Tierra (SSOT) is an high resolution, space-based Earth Observation System ordered by the Chilean Ministry of Defense (MoD). The Chilean MoD and EADS Astrium signed a contract covering development of the system on August 7, 2008.
In addition to the spacecraft, the SSOT also includes a ground control segment and image processing facilities to be located in Chile.
The SSOT is equipped with a latest-generation payload capable of supplying images with a resolution of 1.45 meters in panchromatic mode and 5.8 meters in each of four color bands in multispectral mode. It is intended to serve both military and civil customers using high quality images for applications such as cartography; agricultural management; forestry; water, mineral and oil resources; crop protection; natural disaster response; and urban planning.
Launch Vehicle:
[table="head"]{colsp=2}Characteristics
Soyuz-2.1a
Prime contractor:
|- Samara Space Sentre (Energia Holding enterprise)
GRAU Index:
|- 14A14
Height:
| 51.1 mDiameter:
| max 10.3 mLiftoff mass:
| 313 metric tonnesPayload mass:
| up to 6830 kg (a launch to LEO from Plesetsk)1st stage (boosters B, V, G, D):
|- 4 X RD-107 engines
- Propellants (T-1 Kerosene and LOX)
- Thrust/ISP in vacuum - / 320.2 s
- Thrust/ISP at sea level 85.6 tonnes / 263.3 s
2nd stage (core A):
|- 1 X RD-108 engine
- Propellants (T-1 Kerosene and LOX)
- Thrust/ISP in vacuum 94 tonnes / 320.6 s
- Thrust/ISP at sea level 80.8 tonnes / 257.7 s
3rd stage (block I):
|- 1 X RD-0110 engine
- Propellants (T-1 Kerosene and LOX)
- Thrust/ISP in vacuum 30.38 tonnes / 326 s
Upper Stage:
|
- GRAU Index: -
- Common Name: Fregat (meaning Frigate)
- Designer & Manufacturer: Lavochkin Association (NPO)
- Dimensions: Length 2.4 m, Diameter (max) 3.350 m
- Empty Mass 930 kg
- Propellants 5250 kg max
- Main Engine: 1 X S5.92
- Thrust in vacuum 2.0 tonnes of force (full power)
- Thrust in vacuum 1.4 tonnes of force (small power)
- ISP 333.2 s
Payload Fairing:
|- Diameter 3.7 m
- Length 7.7 m
[/table]
[/table]
The launch vehicle's reliability standings
According to http://www.spacelaunchreport.com/log2011.html#rate:
Code:
================================================================
Vehicle Successes/Tries Realzd Pred Consc. Last Dates
Rate Rate* Succes Fail
================================================================
Soyuz 2-1a/Fregat 6 7# .86 .78 4 5/21/09 2006-
Ascent profile
Weather Forecast for Sinnamary, French Guiana on December 17, 2011 (11 p.m.)
11 PM|24°C|24°C|24°|0 Low|23°C|93%|40%|0%|44%|16KM|NNE 1mph|
References
http://www.esa.int
http://www.cnes.fr
http://www.arianespace.com
http://forum.nasaspaceflight.com
http://www.novosti-kosmonavtiki.ru
http://astronautique.actifforum.com
http://www.spacelaunchreport.com
http://www.cnes.fr/web/CNES-en/3236-pleiades.php
http://www.defense.gouv.fr/dga/actu...au-domaine-du-renseignement-spatial-militaire
http://www.samspace.ru
http://www.laspace.ru
http://www.intellicast.com
http://www.good-stuff.co.uk/suntimes/sunmap.php
Last edited:
