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Information message about launch progress
"Proton-M", "Breeze-M", "Inmarsat-5 F3"
Document: 11. Total: 12
Create: 29.08.2015 09:47:53 (MDT)
Summary SC launch information
¹ |
Event of flight cyclogram |
Predicted flight time |
Data |
Measuring values |
||
[h:m:s from L-OC] |
[s from L-OC] |
time [s from L-OC] |
deviation [s] |
|||
1 |
Gyroplatform activation end |
14:43:54.99 |
-5.01 |
Proton-M |
-5.01 |
0.00 |
2 |
SE1 ignition |
14:43:58.24 |
-1.76 |
Proton-M |
-1.77 |
0.01 |
3 |
Lift-off contact |
14:44:00.00 |
0.00 |
Proton-M |
0.00 |
0.00 |
4 |
SE2 ignition |
14:45:55.38 |
115.38 |
Proton-M |
114.69 |
0.69 |
5 |
Stage 1-2 separation |
14:45:59.63 |
119.63 |
Proton-M |
119.77 |
0.14 |
6 |
VE3 ignition |
14:49:23.78 |
323.78 |
Proton-M |
324.34 |
0.56 |
7 |
SE2 burnout |
14:49:26.48 |
326.48 |
Proton-M |
327.06 |
0.58 |
8 |
Stage 2-3 separation |
14:49:27.18 |
327.18 |
Proton-M |
327.78 |
0.60 |
9 |
SE3 ignition |
14:49:29.58 |
329.58 |
Proton-M |
330.20 |
0.62 |
10 |
HF jettison |
14:49:44.98 |
344.98 |
Proton-M |
345.54 |
0.56 |
11 |
Fairing jettison indication |
14:49:46.88 |
346.88 |
Proton-M |
345.64 |
1.24 |
12 |
Preliminary command |
14:53:30.13 |
570.13 |
Proton-M |
570.95 |
0.82 |
13 |
Main command |
14:53:42.06 |
582.06 |
Proton-M |
582.06 |
0.00 |
14 |
OU separation |
14:53:42.22 |
582.22 |
Proton-M |
582.19 |
0.03 |
15 |
US ICE 1- ignition |
14:55:02.22 |
662.22 |
Breeze-M |
662.70 |
0.48 |
16 |
US SE 1- ignition |
14:55:16.22 |
676.22 |
Breeze-M |
676.59 |
0.37 |
17 |
US ICE 1- burnout |
14:55:18.12 |
678.12 |
Breeze-M |
678.43 |
0.31 |
18 |
US SE 1- burnout |
14:59:42.56 |
942.56 |
Breeze-M |
939.26 |
3.30 |
19 |
US ICE 2- ignition |
16:34:10.00 |
6610.00 |
Breeze-M |
6610.22 |
0.22 |
20 |
US SE 2- ignition |
16:34:30.00 |
6630.00 |
Breeze-M |
6630.15 |
0.15 |
21 |
US ICE 2- burnout |
16:34:31.90 |
6631.90 |
Breeze-M |
6632.24 |
0.34 |
22 |
US SE 2- burnout |
16:54:04.14 |
7804.14 |
Ball center |
7826.60 |
22.46 |
23 |
US ICE 3- ignition |
19:07:25.00 |
15805.00 |
Breeze-M |
15805.22 |
0.22 |
24 |
US SE 3- ignition |
19:07:49.00 |
15829.00 |
Breeze-M |
15829.07 |
0.07 |
25 |
US ICE 3- burnout |
19:07:50.90 |
15830.90 |
Breeze-M |
15831.17 |
0.27 |
26 |
US SE 3- burnout |
19:17:12.73 |
16392.73 |
Breeze-M |
16391.41 |
1.32 |
27 |
US ICE 4- ignition |
19:17:56.93 |
16436.93 |
Breeze-M |
16435.71 |
1.22 |
28 |
APT separation |
19:18:02.73 |
16442.73 |
Breeze-M |
16441.57 |
1.16 |
29 |
US ICE 4- burnout |
19:18:04.93 |
16444.93 |
Breeze-M |
16443.57 |
1.36 |
30 |
US ICE 5- ignition |
19:19:21.73 |
16521.73 |
Breeze-M |
16521.95 |
0.22 |
31 |
US SE 4- ignition |
19:19:29.73 |
16529.73 |
Breeze-M |
16530.08 |
0.35 |
32 |
US ICE 5- burnout |
19:19:31.63 |
16531.63 |
Breeze-M |
16531.92 |
0.29 |
33 |
US SE 4- burnout |
19:27:56.59 |
17036.59 |
Breeze-M |
17031.59 |
5.00 |
34 |
US ICE 6- ignition |
05:58:55.00 |
54895.00 |
Breeze-M |
54895.15 |
0.15 |
35 |
US SE 5- ignition |
05:59:05.00 |
54905.00 |
Breeze-M |
54905.11 |
0.11 |
36 |
US ICE 6- burnout |
05:59:06.90 |
54906.90 |
Breeze-M |
54907.21 |
0.31 |
37 |
US SE 5- burnout |
06:02:34.34 |
55114.34 |
Breeze-M |
55113.02 |
1.32 |
38 |
"Inmarsat-5 F3" SC separation |
06:15:00.00 |
55860.00 |
Breeze-M |
55841.06 |
18.94 |
39 |
US ICE 7- ignition |
09:24:20.00 |
67220.00 |
Breeze-M |
67220.14 |
0.14 |
40 |
US ICE 7- burnout |
09:24:35.00 |
67235.00 |
Breeze-M |
67235.35 |
0.35 |
41 |
US ICE 8- ignition |
10:34:10.00 |
71410.00 |
No date |
||
42 |
US ICE 8- burnout |
10:35:50.00 |
71510.00 |
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.Preliminary orbit parameter estimation per US "Breeze-M"
MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.08.2015 14:53:42 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:21:17.7 |
1:21:16.8 |
0:0:1.0 |
----------- |
------------------- |
2 |
i |
51 °32 '29 " |
51 °32 '52 " |
0 °0 '23 " |
----------- |
------------------- |
3 |
Hp [km] |
-486.91 |
-488.35 |
1.44 |
----------- |
------------------- |
4 |
Ha [km] |
177.70 |
177.49 |
0.20 |
----------- |
------------------- |
Parking orbit.Preliminary orbit parameter estimation per US "Breeze-M"
MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.08.2015 14:59:52 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
1:27:56.9 |
1:27:56.8 |
0:0:0.1 |
----------- |
------------------- |
2 |
i |
51 °32 '46 " |
51 °33 '10 " |
0 °0 '24 " |
----------- |
------------------- |
3 |
Hp [km] |
179.90 |
180.00 |
0.10 |
----------- |
------------------- |
4 |
Ha [km] |
180.25 |
180.00 |
0.25 |
----------- |
------------------- |
Intermediate orbit.Preliminary orbit parameter estimation per US "Breeze-M"
MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.08.2015 16:54:14 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
2:34:13.0 |
2:34:12.1 |
0:0:0.8 |
----------- |
------------------- |
2 |
i |
51 °0 '2 " |
51 °0 '0 " |
0 °0 '2 " |
----------- |
------------------- |
3 |
Hp [km] |
301.72 |
302.00 |
0.28 |
----------- |
------------------- |
4 |
Ha [km] |
6008.39 |
6006.99 |
1.40 |
----------- |
------------------- |
Transfer orbit.Preliminary orbit parameter estimation per US "Breeze-M"
MDT of orbit.parameters ( day.month.year hour:min:sec) - 28.08.2015 19:28:06 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
21:24:30.1 |
21:24:14.8 |
0:0:15.3 |
----------- |
------------------- |
2 |
i |
50 °30 '13 " |
50 °30 '0 " |
0 °0 '13 " |
----------- |
------------------- |
3 |
Hp [km] |
481.12 |
482.00 |
0.89 |
----------- |
------------------- |
4 |
Ha [km] |
65062.14 |
65050.89 |
11.25 |
----------- |
------------------- |
"Inmarsat-5 F3" target orbit.Preliminary orbit parameter estimation per US "Breeze-M"
MDT of orbit.parameters ( day.month.year hour:min:sec) - 29.08.2015 06:02:44 | ||||||
¹ |
Parameter |
Estimation |
Nominal |
Deviation |
Limit |
Comment |
1 |
T [h.m.s] |
22:59:21.0 |
22:59:22.5 |
0:0:1.4 |
----------- |
------------------- |
2 |
i |
26 °51 '44 " |
26 °44 '57 " |
0 °6 '47 " |
----------- |
------------------- |
3 |
Hp [km] |
4331.08 |
4345.12 |
14.05 |
----------- |
------------------- |
4 |
Ha [km] |
65020.01 |
65006.92 |
13.09 |
----------- |
------------------- |
Used abbreviations and notation:
| MBC - Main Ballistic Center |
| SDO MEI - Special Design Office MEI |
| SSC - Space Surveillance Center |
| T - orbital period |
| i - inclination |
| Hp - perigee altitude |
| Ha - apogee altitude |
Screen shots:
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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Video |
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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 |