K H R U N I C H E V T E L E C O M C o m p a n y Launch information processing and display center |
Information message about launch progress
"Rockot", "Breeze-KM", "SMOS"
Document: 2. Total: 9
Create: 02.11.2009 05:00:24 (MDT)
Launch vehicle powered flight and sub-orbital trajectory parameters
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 |
-00:00:14.045 |
-14.045 |
Rockot |
-14.045 |
0.000 |
2 |
SE1 ignition |
-00:00:02.845 |
-2.845 |
Rockot |
-3.145 |
0.300 |
3 |
Lift-off contact |
00:00:00.000 |
0.000 |
Rockot |
0.000 |
0.000 |
4 |
StE2 ignition |
00:01:58.025 |
118.025 |
Rockot |
118.050 |
0.025 |
5 |
SE1 burnout |
00:02:00.525 |
120.525 |
Rockot |
120.450 |
0.075 |
6 |
Stage 1-2 separation |
00:02:02.225 |
122.225 |
Rockot |
122.220 |
0.005 |
7 |
SE2 ignition |
00:02:04.575 |
124.575 |
No date |
||
8 |
HF jettison |
00:02:43.044 |
163.044 |
Rockot |
162.950 |
0.094 |
9 |
Preliminary command |
00:04:44.085 |
284.085 |
Rockot |
283.950 |
0.135 |
10 |
Main command |
00:05:03.955 |
303.955 |
Rockot |
304.050 |
0.095 |
11 |
OU separation |
00:05:04.955 |
304.955 |
Rockot |
305.050 |
0.095 |
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 |
Screen shots:
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
Video |
|
1-st stage separation |
|
HF jettison |
|
US separation |