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Information message about launch progress
"Proton-M", "Breeze-M", "Astra-2G"

Document: 11. Total: 12
Create: 28.12.2014 12:47:04 (MDT)


Summary SC launch information

¹

Event of flight cyclogram

Predicted flight time

Data
source

Measuring values

[h:m:s from L-OC]

[s from L-OC]

time [s from L-OC]

deviation [s]

1

Gyroplatform activation end

00:37:43.99

-5.01

Proton-M

-5.01

0.00

2

SE1 ignition

00:37:47.24

-1.76

Proton-M

-1.77

0.01

3

Lift-off contact

00:37:49.00

0.00

Proton-M

0.00

0.00

4

SE2 ignition

00:39:44.38

115.38

Proton-M

114.66

0.72

5

Stage 1-2 separation

00:39:48.63

119.63

Proton-M

118.85

0.78

6

VE3 ignition

00:43:12.78

323.78

Proton-M

323.91

0.13

7

SE2 burnout

00:43:15.48

326.48

Proton-M

326.63

0.15

8

Stage 2-3 separation

00:43:16.18

327.18

Proton-M

327.35

0.17

9

SE3 ignition

00:43:18.58

329.58

Proton-M

329.78

0.20

10

HF jettison

00:43:33.98

344.98

Proton-M

345.11

0.13

11

Fairing jettison indication

00:43:35.88

346.88

Proton-M

345.21

1.67

12

Preliminary command

00:47:19.13

570.13

Proton-M

570.75

0.62

13

Main command

00:47:31.06

582.06

Proton-M

581.70

0.36

14

OU separation

00:47:31.22

582.22

Proton-M

581.83

0.39

15

US ICE 1- ignition

00:48:51.22

662.22

Breeze-M

662.18

0.04

16

US SE 1- ignition

00:49:05.22

676.22

Breeze-M

676.33

0.11

17

US ICE 1- burnout

00:49:07.12

678.12

Breeze-M

678.04

0.08

18

US SE 1- burnout

00:53:35.81

946.81

Breeze-M

940.31

6.50

19

US ICE 2- ignition

01:45:02.00

4033.00

Breeze-M

4033.35

0.35

20

US SE 2- ignition

01:45:22.00

4053.00

Breeze-M

4053.27

0.27

21

US ICE 2- burnout

01:45:23.90

4054.90

Breeze-M

4055.37

0.47

22

US SE 2- burnout

02:03:05.93

5116.93

Breeze-M

5099.49

17.44

23

US ICE 3- ignition

04:05:37.00

12468.00

Breeze-M

12468.09

0.09

24

US SE 3- ignition

04:06:01.00

12492.00

Breeze-M

12492.21

0.21

25

US ICE 3- burnout

04:06:02.90

12493.90

Breeze-M

12494.04

0.14

26

US SE 3- burnout

04:17:30.33

13181.33

Breeze-M

13176.67

4.66

27

US ICE 4- ignition

04:18:14.53

13225.53

Breeze-M

13220.97

4.56

28

APT separation

04:18:20.33

13231.33

Breeze-M

13226.84

4.49

29

US ICE 4- burnout

04:18:22.53

13233.53

Breeze-M

13229.10

4.43

30

US ICE 5- ignition

04:19:39.33

13310.33

Breeze-M

13310.36

0.03

31

US SE 4- ignition

04:19:47.33

13318.33

Breeze-M

13318.49

0.16

32

US ICE 5- burnout

04:19:49.23

13320.23

Breeze-M

13320.58

0.35

33

US SE 4- burnout

04:25:40.46

13671.46

Breeze-M

13666.35

5.11

34

US ICE 6- ignition

09:30:47.00

31978.00

Breeze-M

31978.10

0.10

35

US SE 5- ignition

09:30:57.00

31988.00

Breeze-M

31988.12

0.12

36

US ICE 6- burnout

09:30:58.90

31989.90

Breeze-M

31990.22

0.32

37

US SE 5- burnout

09:37:12.32

32363.32

Breeze-M

32361.94

1.38

38

"Astra-2G" SC separation

09:49:49.00

33120.00

Breeze-M

33120.39

0.39

39

US ICE 7- ignition

11:54:29.00

40600.00

Breeze-M

40600.14

0.14

40

US ICE 7- burnout

11:54:41.00

40612.00

Breeze-M

40612.14

0.14

41

US ICE 8- ignition

13:14:29.00

45400.00

No date

42

US ICE 8- burnout

13:16:09.00

45500.00

No date

Used abbreviations:

APT- Additional propellant tank    ETC- Engine thrust control
F- Fuel    GS- Gyro Settings
GTSV- Ground Tracking Stations Visibility
HF- Head fairing    ICE- US impulse correction engine
L-OC- Lift-Off contact    MC- Main command
MDT- Moscow Decree time    ND- Nominal duty
NTL- Nomihal thrust level    O- Oxidant
ODCC- Onboard digital computer complex    OU- Orbital unit
PC- Preliminary command    PU- Propulsion unit
SC- Spacecraft    SHU- Spacehead unit
SE- Sustainer engine    SEU- Sustainer engine unit
StE- Stabilization engine    US- Upper stage
UTC- Universal Coordinated Time    VE- Vernier engine

Sub-orbital trajectory.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.12.2014 00:47:31

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

1:21:17.0

1:21:16.8

0:0:0.2

-----------

-------------------

2

a [km]

6215.74

6215.57

0.16

-----------

-------------------

3

e

0.0535716

0.0535623

0.0000093

-----------

-------------------

4

i

51 °33 '17 "

51 °32 '52 "

0 °0 '25 "

-----------

-------------------

5

Hp [km]

-495.39

-495.48

0.10

-----------

-------------------

6

Ha [km]

170.59

170.36

0.23

-----------

-------------------

Parking orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.12.2014 00:53:45

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

1:27:59.1

1:27:59.2

0:0:0.2

-----------

-------------------

2

a [km]

6552.86

6553.00

0.14

-----------

-------------------

3

e

0.0000387

0.0000001

0.0000386

-----------

-------------------

4

i

51 °33 '35 "

51 °33 '10 "

0 °0 '24 "

-----------

-------------------

5

Hp [km]

174.47

174.86

0.39

-----------

-------------------

6

Ha [km]

174.98

174.86

0.12

-----------

-------------------

Intermediate orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.12.2014 02:03:15

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

2:21:55.6

2:21:55.6

0:0:0.1

-----------

-------------------

2

a [km]

9013.04

9013.00

0.04

-----------

-------------------

3

e

0.2624098

0.2623986

0.0000113

-----------

-------------------

4

i

50 °18 '27 "

50 °17 '60 "

0 °0 '27 "

-----------

-------------------

5

Hp [km]

269.79

269.86

0.07

-----------

-------------------

6

Ha [km]

5000.01

4999.86

0.15

-----------

-------------------

Transfer orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.12.2014 04:25:50

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

10:35:25.9

10:35:3.8

0:0:22.1

-----------

-------------------

2

a [km]

24483.46

24473.98

9.48

-----------

-------------------

3

e

0.7217301

0.7216227

0.0001074

-----------

-------------------

4

i

49 °5 '53 "

49 °6 '0 "

0 °0 '7 "

-----------

-------------------

5

Hp [km]

434.88

434.87

0.01

-----------

-------------------

6

Ha [km]

35775.78

35756.83

18.95

-----------

-------------------

"Astra-2G" target orbit.Final orbit parameter estimation per MBC

MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.12.2014 09:37:22

¹

Parameter

Estimation

Nominal

Deviation

Limit

Comment

1

T [h.m.s]

11:48:5.7

11:48:34.3

0:0:28.6

-----------

-------------------

2

a [km]

26316.08

26327.90

11.82

-----------

-------------------

3

e

0.6007782

0.5995909

0.0011872

-----------

-------------------

4

i

22 °58 '41 "

23 °0 '0 "

0 °1 '19 "

-----------

-------------------

5

Hp [km]

4127.82

4163.79

35.97

-----------

-------------------

6

Ha [km]

35748.08

35735.73

12.34

-----------

-------------------

Used abbreviations and notation:

MBC          - Main Ballistic Center
SDO MEI   - Special Design Office MEI
SSC           - Space Surveillance Center
T               - orbital period
a               - semi-major axis
e               - eccentricity
i                - inclination
Hp             - perigee altitude
Ha             - apogee altitude

Screen shots:

Video
Video
Video
Video
Video
Video
Video
Video
Video
Video
1-st stage separation
First stage impact area
2-nd stage separation
HF jettison
Second stage and HF impact area
US separation
End of booster phase
End of booster phase
End of booster phase
End of booster phase
US main engine action 1-st ign. (ICE)
US main engine action (1-st ign.)
US main engine action (2-nd ign.)
US main engine action (3-rd ign.)
APT separation
US main engine action (4-th ign.)
US main engine action (5-th ign.)
SC separation
SC separation
SC separation
US withdrawel

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