T-0:00:05.0 |
Engine start |
 |
The
RS-68 main engine begins to ignite as the liquid hydrogen fuel valve is
opened, creating a large fireball at the base of the rocket. The engine
powers up to full throttle for a computer-controlled checkout before
liftoff. |
|
T-0:00:00.0 |
Liftoff |
 |
The
rocket's two strap-on solid rocket motors are lit, the four hold-down
bolts are released and the Delta 4 lifts off from Cape Canaveral's pad
37B. The pad's three swing arms retract at T-0 seconds. |
|
T+0:01:00.7 |
Max-Q |
 |
The
vehicle experiences the region of maximum dynamic pressure. Both solid
motors and the RS-68 liquid hydrogen/liquid oxygen engine continue to
fire as the vehicle heads downrange, arcing over the Atlantic along a
45-degree flight azimuth. |
|
T+0:01:40.0 |
Jettison solid motors |
 |
Having
used up all their solid-propellant and experienced burnout six seconds
ago, the two strap-on boosters are jettisoned from the Delta's first
stage. The spent casings fall into the ocean. |
|
T+0:04:07.2 |
Main engine cutoff |
 |
The hydrogen-fueled RS-68 rocket engine completes its firing and shuts down to finish the first stage burn. |
|
T+0:04:14.5 |
Stage separation |
 |
The
Common Booster Core first stage and the attached interstage are
separated in one piece from the Delta 4's upper stage. The upper stage
engine's extendible nozzle drops into position as the first stage
separates. |
|
T+0:04:29.0 |
Second stage ignition |
 |
The
upper stage begins its job to place the GPS 2F-6 satellite into space
with the first of two firings by the RL10B-2 liquid hydrogen/liquid
oxygen engine. |
|
T+0:04:39.5 |
Jettison payload fairing |
 |
The
four-meter diameter composite payload fairing that protected the GPS
2F-6 cargo atop the Delta 4 during the atmospheric ascent is no longer
needed, allowing it to be jettisoned in two halves. |
|
T+0:15:31.5 |
Upper stage shutdown |
 |
The
RL10 upper stage engine shuts down to complete its first firing of the
launch. The rocket and attached satellite reach an intermediate transfer
orbit where it coasts for the next three hours. |
|
T+3:03:25.0 |
Restart upper stage |
 |
The upper stage reaches the proper point in space and reignites the the RL10 engine to circularize the orbit. |
|
T+3:05:08.2 |
Upper stage shutdown |
 |
The
powered phase of the Delta 4's mission to reach the GPS constellation
concludes. The targeted circular orbit is 11,047 nautical miles with an
inclination of 55 degrees. |
|
T+3:15:49.5 |
Separate spacecraft |
 |
The GPS 2F-6 satellite is released into space from the Delta 4 rocket to upgrade the orbiting navigation network. |
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