October 23, 2017

Timeline: Delta 4/WGS 9 launch events

Follow the Delta 4 rocket’s ascent into orbit from Cape Canaveral’s Complex 37 launch pad to deploy the Wideband Global SATCOM 9 communications satellite. Liftoff is scheduled for Saturday at 7:44 p.m. EDT (2344 GMT).

T-00:05.0 Engine start

The RS-68A 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-00:00.0 Liftoff

The rocket’s four 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+00:46.1 Max-Q

The vehicle experiences the region of maximum dynamic pressure. The solid motors and the RS-68A liquid hydrogen/liquid oxygen engine continue to fire as the vehicle heads downrange, arcing over the Atlantic along a 93.46-degree flight azimuth.

T+01:40.1 Jettison solid motors

Having used up all their solid-propellant and experienced burnout eight seconds ago, the two strap-on boosters with fixed nozzles are jettisoned from the Delta’s first stage, followed two seconds later by the pair of boosters with steerable nozzles.

T+03:14.6 Jettison payload fairing

The five-meter diameter composite payload fairing that protected the WGS 9 cargo atop the Delta 4 during the atmospheric ascent is no longer needed, allowing it to be jettisoned in two halves.

T+03:56.5 Main engine cutoff

The hydrogen-fueled RS-68A rocket engine completes its burn and shuts down to complete the first stage of flight.

T+04:03.1 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+04:16.1 Second stage ignition

The upper stage begins its job to place the WGS 9 satellite into space with the first of two firings by the RL10B-2 liquid hydrogen/liquid oxygen engine.

T+19:53.6 Upper stage shutdown

The RL10 upper stage engine shuts down to complete its first firing of the launch. The rocket and attached satellite reach a parking orbit.

T+29:26.6 Restart upper stage

After a short coast period, the upper stage is reignited to raise the orbit to the planned altitude for deploying the payload.

T+32:35.3 Upper stage shutdown

The powered phase of the Delta 4’s mission to loft WGS 8 concludes. The second burn will reach the planned super-synchronous orbit of 270 by 27,572 statute miles with an inclination of 27 degrees.

T+41:45.6 Separate spacecraft

The Wideband Global SATCOM 9 military communications satellite is released into space from the Delta 4 rocket. The Boeing-built satellite will use its onboard propulsion to reach geostationary orbit where it will match Earth’s rotation and appear fixed above the equator in the WGS constellation.

After performing its mission, the upper stage will perform a 10-second deorbit burn 30 minutes after spacecraft separation. Any debris surviving reentry will impact the Pacific about 12 hours after launch.

See earlier WGS 9 coverage.

Our Delta archive.

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