T-00:00 |
Liftoff |
The Delta 2 rocket's main engine and twin vernier steering thrusters are started moments before launch. The six ground-start strap-on solid rocket motors are ignited at T-0 to begin the mission. |
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T+01:16.4 |
Ground SRM Burnout |
The six ground-start Alliant TechSystems-built solid rocket motors consume all their propellant and burn out. |
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T+01:19.0 |
Air-Lit SRM Ignition |
The three remaining solid rocket motors strapped to the Delta 2 rocket's first stage are ignited. |
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T+01:20.5 |
Jettison Ground SRMs |
The six spent ground-started solid rocket boosters are jettisoned in sets of three to fall into the Atlantic Ocean. |
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T+02:39.5 |
Jettison Air-Lit SRMs |
Having burned out, the three spent air-started solid rocket boosters are jettisoned toward the Atlantic Ocean. |
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T+04:23.5 |
Main Engine Cutoff |
After consuming its RP-1 fuel and liquid oxygen, the Rocketdyne RS-27A first stage main engine is shut down. The vernier engines cut off moments later. |
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T+04:31.5 |
Stage Separation |
The Delta rocket's first stage is separated now, having completed its job. The spent stage will fall into the Atlantic Ocean. |
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T+04:37.0 |
Second Stage Ignition |
With the stage jettisoned, the rocket's second stage takes over. The Aerojet AJ118-K liquid-fueled engine ignites for the first of two firings needed to place the upper stage and MESSENGER satellite into the proper orbit. |
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T+04:41.0 |
Jettison Payload Fairing |
The 9.5-foot diameter payload fairing that protected the MESSENGER satellite atop the Delta 2 during the atmospheric ascent is jettisoned is two halves. |
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T+08:49.0 |
Second Stage Cutoff 1 |
The second stage engine shuts down to complete its first firing of the launch. The rocket and attached MESSENGER spacecraft are now in a coast period before the second stage reignites. The orbit achieved should be 90 miles circular and inclined 32.44 degrees. |
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T+46:01.0 |
Second Stage Restart |
Delta's second stage engine reignites to raise the orbit. |
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T+48:52.3 |
Second Stage Cutoff 2 |
The second stage shuts down after a near-three-minute firing. The orbit achieved should be 4,136.6 miles at apogee, 84.2 miles at perigee and inclined 32.49 degrees. |
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T+49:33.2 |
Spin Up |
Tiny thrusters on the side of the rocket will be fired to spin up the vehicle in preparation for stage separation. |
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T+49:35.3 |
Stage Separation |
The liquid-fueled second stage is jettisoned from the rest of the Delta 2 rocket. |
|
T+50:14.1 |
Third Stage Ignition |
The Thiokol Star 48B solid-fueled third stage is then ignited to propel the MESSENGER satellite into orbit around the Sun. |
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T+51:39.3 |
Third Stage Burnout |
Having used up all its solid-propellant, the third stage burns out to completed the powered phase of the launch sequence for MESSENGER. |
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T+56:43.7 |
Spacecraft Separation |
NASA's MESSENGER space probe is released into space from the Delta 2 rocket for its five billion mile journey from Earth to the solar system's innermost planet -- Mercury. |