 | |
| Mission Time (hh:mm) |
Event |
Description |
Orbit (perigee x apogee, km) |
| 00:00 |
Launch |
RSRM ignition, liftoff |
. |
| 00:02 |
SRB Sep |
RSRM burnout, separation |
. |
| 00:08 |
MECO |
Main engine cutoff |
. |
| 00:08 |
ET Sep |
External Tank separation |
20? x 320 |
| 00:45 |
OMS-2 |
OMS orbit circ burn |
320 x 320 |
| 02:00 |
PLBD |
Payload bay doors open |
. |
| 06:29 |
Tilt |
Raise tilt table to 4 deg |
. |
| 07:29 |
Tilt |
Raise tilt table to 29 deg |
. |
| 08:00 |
. |
Chandra to internal power |
. |
| 08:32 |
Tilt |
Raise tilt table to 58 deg |
. |
| 08:42 |
Deploy |
Chandra/IUS-27 deploy |
320 x 320 |
| 09:32 |
LGA |
Chandra deploys LGA antenna |
. |
| 09:41 |
SRM-1 |
IUS-27 SRM-1 burn |
. |
| 09:43 |
SRM-1 cutoff |
IUS-27 SRM-1 sep from SRM-2 |
320 x ? |
| 09:46 |
SRM-2 |
IUS-27 SRM-2 burn |
. |
| 09:48 |
SRM-2 cutoff |
IUS-27 SRM-2 cutoff |
320 x 64000 |
| 10:11 |
SA Deploy |
Chandra solar panels deploy |
. |
| 10:58 |
SRM-2 sep |
IUS-27 SRM-2 sep from Chandra |
. |
| 42:30 |
IPS-1 |
IPS burn 1, perigee |
320 x 89900 |
| 81:51 |
IPS-2 |
IPS burn 2, perigee |
320 x 140000 |
| 111:09 |
IPS-3 |
IPS burn 3, apogee |
10000 x 140000 |
| 174:52 |
IPS-4 |
Trim burn, apogee |
10000 x 140000 |
|
