אינדקס
לווין קנדי הישוגר 17 למאי מביקנור בקזחסטן
32 טנספונדרים בתחום KU BAND
מיקום הלווין 91W
http://nimiq6.imgondemand.com/streamFlash.aspx
Lift-off at 2:36 , also check out 8:03
tv-tsenki.com coverage of Proton Briz-M carrying Nimiq 6 launch
הפרדה ראשונה בוצע בהצלחה
We have had a successful mission with the ILS Proton Rocket carrying the Nimiq 6 satellite built by Space Systems/Loral. We have had confirmation that the Nimiq 6 satellite separated from the...
Nimiq 6 | Third and Fourth Burn May 17, 2012 | 0 comments |
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We have confirmed that the Breeze M upper stage has successfully completed its 3rd & 4th burns, as well as jettisoning its additional propellant tank. The vehicle is now in a 5-hour coast...
Nimiq 6 | Second Burn May 17, 2012 | 0 comments |
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As the Breeze M upper stage of our Proton M rocket continues its climb into space with the Nimiq 6 satellites onboard, we have received confirmation that the 2nd burn of the upper stage occurred...
Nimiq 6 | First Burn May 17, 2012 | 0 comments |
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We have received confirmation of completion of the first burn. The vehicle is now scheduled to be out of range for about an hour, after which we will hear confirmation of the second burn.
Nimiq 6 | Stage Separations May 17, 2012 | 0 comments |
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We had a successful liftoff about 11 minutes ago of our Proton M Breeze M rocket, which is carrying the Nimiq 6 satellite on board. The three stages of the Proton vehicle have performed as planned...
Nimiq 6 | Liftoff! May 17, 2012 | 0 comments |
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We have liftoff! of the Proton M Breeze M rocket and the Nimiq 6 satellite.
Nimiq 6 | New Home on Pad 24… Check! May 14, 2012 | 0 comments |
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Yesterday was a long and exciting day here in Baikonur. After receiving the OK last night from the State Commission it was time to send the Nimiq 6 ILV on its trip to Launch Pad 24.
...
Nimiq 6 | Russian Holiday During the Campaign… Check! May 9, 2012 | 0 comments |
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It is May 9, and this is one of the most memorialized days in Russian History. It is Victory Day, the day that marks the end of World War II. Just as Memorial Day is in America, this...
Nimiq 6 | Putting It All Together... Check! May 8, 2012 | 0 comments |
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As we get closer to our launch date, the number of activities is increasing...
One of the more “technical” operations that we have to perform is signing the...
Nimiq 6 | Mobile Service Tower May 7, 2012 | 0 comments |
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A great day to head to the 8th floor of the Mobile Service Tower as we conducted a Radio Frequency check between the Control room and Tower simulating the spacecraft. This is essentially a...
ILS PROTON BREEZE M LAUNCH VEHICLE
The ILS Proton Breeze M Specifications
Performance Reference: 6,150 kg to reference PSM at 1,500m/s delta V to GSO
Typical Mission: Approximately 9 hours utilizing a five-burn Breeze M mission design
Stages: Three-stage Proton rocket with restartable upper stage
Structure Type: Monocoque
Materials: Aluminum and composites
Propellants: Nitrogen Tetroxide (N2O4); Unsymmetrical DiMethyl Hydrazine (UDMH)
Gross Liftoff Mass: 705,000 kg (1,554,000 lb)
Total Length: 58.2 m (191 ft), with standard commercial 4.0 m diameter fairing.
The enhanced performance provided by the commercial Proton launch vehicle enables our customers to design and launch heavier and more capable spacecraft while maintaining cost effective mission life times.
Advantages of the ILS Proton Breeze M Launch Vehicle:
Restartable upper stage for mission optimization - LEO, MEO, GTO, GSO, SSTO
Compatible with all major commercial spacecraft platforms for dedicated single and multiple launches
Experience launching dual-use satellites and satellites with hosted payloads
Demonstrated capability to build and serve space stations
ILS Proton Breeze M Rocket Stages:
+ Payload Fairing
+ Payload Adaptor
+ Breeze M
+ Proton 3rd Stage
+ Proton 1st & 2nd Stage
PAYLOAD FAIRING
The Payload Fairing encloses and protects the spacecraft
during ground operations and launch vehicle ascent.
Two PLF lengths are available at 13305 mm and the standard 15255 mm. Although of similar design, there are specific useable volumes for the two fairing types tailored to individual adapter systems. Specific adapters take into account required adapter clearances for installation and required flight clearances with the adapter structure.
Please see Section 4 of the Proton Mission Planner's Guide for further detail
PAYLOAD ADAPTOR
Multiple standard payload adaptors
are available to meet a multitude of
spacecraft mission requirements to
accommodate both mass and volume.
BREEZE M
Length: 2.61 m
Diameter: 4.0 m
Engine(s): One 14D30 Sustainer, Four 11D458M Control Thrusters
Thrust: 19.62 kN
Inert Mass: 2,370 kg
Propellant: 19,800 kg
Mass: Comprised of a central core and an additional
jettisonable propellant tank and powered by one
pump-fed gimballed main engine.Features increased
lift capability of 6,150 kg (13,558 lb) PSM to
geosynchronous transfer orbit with a 1,500 m/sec
residual velocity to GSO. Strengthened structure
allows launching heavier spacecraft with higher
center of gravity locations, and even allows for
launching multiple spacecraft.
PROTON 3RD STAGE
Length: 4.11m
Diameter: 4.1m
Engine(s): One RD-0213 and one Four-Nozzle Vernier
Thrust: 583 kN (131,000 lbf)
Inert Mass: 3,500 kg
Propellant: 46,562 kg
Guidance, navigation, and control of the
Proton M during operations of the first three
stages is carried out by a triple redundant closed-loop
digital avionics system mounted in the 3rd Stage
PROTON 1ST AND 2ND STAGE
2nd Stage
Length: 17.05 m
Diameter: 4.1 m
Engine(s): Three RD-0210 and One RD-0211
Thrust: 2.4 MN
Inert Mass: 11,000 kg
Propellant: 157,300 kg
Mass: Utilizes conventional cylindrical design.
1st Stage
Length: 21.18 m
Diameter: 7.4 m
Engine(s): Six RD-276
Thrust: 10.0 MN at Sea Level
Inert Mass: 30,600 kg
Propellant: 428,300 kg
Mass: Consists of a central tank containing
oxidizer surrounded by six outboard
fuel tanks, each of which also carries
one of the six engines.
32 טנספונדרים בתחום KU BAND
מיקום הלווין 91W
http://nimiq6.imgondemand.com/streamFlash.aspx
Lift-off at 2:36 , also check out 8:03
tv-tsenki.com coverage of Proton Briz-M carrying Nimiq 6 launch
הפרדה ראשונה בוצע בהצלחה
We have had a successful mission with the ILS Proton Rocket carrying the Nimiq 6 satellite built by Space Systems/Loral. We have had confirmation that the Nimiq 6 satellite separated from the...
Nimiq 6 | Third and Fourth Burn May 17, 2012 | 0 comments |
Add new comment
We have confirmed that the Breeze M upper stage has successfully completed its 3rd & 4th burns, as well as jettisoning its additional propellant tank. The vehicle is now in a 5-hour coast...
Nimiq 6 | Second Burn May 17, 2012 | 0 comments |
Add new comment
As the Breeze M upper stage of our Proton M rocket continues its climb into space with the Nimiq 6 satellites onboard, we have received confirmation that the 2nd burn of the upper stage occurred...
Nimiq 6 | First Burn May 17, 2012 | 0 comments |
Add new comment
We have received confirmation of completion of the first burn. The vehicle is now scheduled to be out of range for about an hour, after which we will hear confirmation of the second burn.
Nimiq 6 | Stage Separations May 17, 2012 | 0 comments |
Add new comment
We had a successful liftoff about 11 minutes ago of our Proton M Breeze M rocket, which is carrying the Nimiq 6 satellite on board. The three stages of the Proton vehicle have performed as planned...
Nimiq 6 | Liftoff! May 17, 2012 | 0 comments |
Add new comment
We have liftoff! of the Proton M Breeze M rocket and the Nimiq 6 satellite.
Nimiq 6 | New Home on Pad 24… Check! May 14, 2012 | 0 comments |
Add new comment
Yesterday was a long and exciting day here in Baikonur. After receiving the OK last night from the State Commission it was time to send the Nimiq 6 ILV on its trip to Launch Pad 24.
...
Nimiq 6 | Russian Holiday During the Campaign… Check! May 9, 2012 | 0 comments |
Add new comment
It is May 9, and this is one of the most memorialized days in Russian History. It is Victory Day, the day that marks the end of World War II. Just as Memorial Day is in America, this...
Nimiq 6 | Putting It All Together... Check! May 8, 2012 | 0 comments |
Add new comment
As we get closer to our launch date, the number of activities is increasing...
One of the more “technical” operations that we have to perform is signing the...
Nimiq 6 | Mobile Service Tower May 7, 2012 | 0 comments |
Add new comment
A great day to head to the 8th floor of the Mobile Service Tower as we conducted a Radio Frequency check between the Control room and Tower simulating the spacecraft. This is essentially a...
ILS PROTON BREEZE M LAUNCH VEHICLE
The ILS Proton Breeze M Specifications
Performance Reference: 6,150 kg to reference PSM at 1,500m/s delta V to GSO
Typical Mission: Approximately 9 hours utilizing a five-burn Breeze M mission design
Stages: Three-stage Proton rocket with restartable upper stage
Structure Type: Monocoque
Materials: Aluminum and composites
Propellants: Nitrogen Tetroxide (N2O4); Unsymmetrical DiMethyl Hydrazine (UDMH)
Gross Liftoff Mass: 705,000 kg (1,554,000 lb)
Total Length: 58.2 m (191 ft), with standard commercial 4.0 m diameter fairing.
The enhanced performance provided by the commercial Proton launch vehicle enables our customers to design and launch heavier and more capable spacecraft while maintaining cost effective mission life times.
Advantages of the ILS Proton Breeze M Launch Vehicle:
Restartable upper stage for mission optimization - LEO, MEO, GTO, GSO, SSTO
Compatible with all major commercial spacecraft platforms for dedicated single and multiple launches
Experience launching dual-use satellites and satellites with hosted payloads
Demonstrated capability to build and serve space stations
ILS Proton Breeze M Rocket Stages:
+ Payload Fairing
+ Payload Adaptor
+ Breeze M
+ Proton 3rd Stage
+ Proton 1st & 2nd Stage
PAYLOAD FAIRING
The Payload Fairing encloses and protects the spacecraft
during ground operations and launch vehicle ascent.
Two PLF lengths are available at 13305 mm and the standard 15255 mm. Although of similar design, there are specific useable volumes for the two fairing types tailored to individual adapter systems. Specific adapters take into account required adapter clearances for installation and required flight clearances with the adapter structure.
Please see Section 4 of the Proton Mission Planner's Guide for further detail
PAYLOAD ADAPTOR
Multiple standard payload adaptors
are available to meet a multitude of
spacecraft mission requirements to
accommodate both mass and volume.
BREEZE M
Length: 2.61 m
Diameter: 4.0 m
Engine(s): One 14D30 Sustainer, Four 11D458M Control Thrusters
Thrust: 19.62 kN
Inert Mass: 2,370 kg
Propellant: 19,800 kg
Mass: Comprised of a central core and an additional
jettisonable propellant tank and powered by one
pump-fed gimballed main engine.Features increased
lift capability of 6,150 kg (13,558 lb) PSM to
geosynchronous transfer orbit with a 1,500 m/sec
residual velocity to GSO. Strengthened structure
allows launching heavier spacecraft with higher
center of gravity locations, and even allows for
launching multiple spacecraft.
PROTON 3RD STAGE
Length: 4.11m
Diameter: 4.1m
Engine(s): One RD-0213 and one Four-Nozzle Vernier
Thrust: 583 kN (131,000 lbf)
Inert Mass: 3,500 kg
Propellant: 46,562 kg
Guidance, navigation, and control of the
Proton M during operations of the first three
stages is carried out by a triple redundant closed-loop
digital avionics system mounted in the 3rd Stage
PROTON 1ST AND 2ND STAGE
2nd Stage
Length: 17.05 m
Diameter: 4.1 m
Engine(s): Three RD-0210 and One RD-0211
Thrust: 2.4 MN
Inert Mass: 11,000 kg
Propellant: 157,300 kg
Mass: Utilizes conventional cylindrical design.
1st Stage
Length: 21.18 m
Diameter: 7.4 m
Engine(s): Six RD-276
Thrust: 10.0 MN at Sea Level
Inert Mass: 30,600 kg
Propellant: 428,300 kg
Mass: Consists of a central tank containing
oxidizer surrounded by six outboard
fuel tanks, each of which also carries
one of the six engines.
נערך לאחרונה על-ידי dimitri82 בתאריך Fri May 18, 2012 8:02 am, סך-הכל נערך 2 פעמים
