| L-minus 8 hours, 15 minutes | Call to Stations | 
| The launch team reports to the control center at NASA's Wallops Flight Facility. | 
	
		
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| L-minus 7 hours, 45 minutes | Begin Launch Checklist | 
	
| The launch team conducts voice checks over radio loops and begins setup of the Range support systems. | 
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| L-minus 6 hours, 30 minutes | Clear the Pad | 
	
| Workers evacuate the launch pad. | 
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| L-minus 6 hours, 5 minutes | Poll to Initiate Loading Sequencer Timeline | 
	
| The launch team conducts a "go/no go" poll to initiate the loading sequencer timeline. | 
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| L-minus 6 hours | Initiate Orbital Commodities Control System Sequencer | 
	
| The Orbital Commodities Control System sequencer begins operating and warm helium charging begins on the Antares rocket's first stage. | 
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| L-minus 5 hours, 55 minutes | Vehicle Power-Up | 
	
| The Antares launch vehicle is powered on using an external power source to begin systems testing. | 
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| L-minus 4 hours, 55 minutes | Poll to Initiate Pre-Launch Processing | 
	
| The launch team is polled for a "go" to begin the pre-launch processing sequence. | 
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| L-minus 3 hours, 40 minutes | Begin First Hold | 
	
| The countdown pauses for 15 minutes to allow Orbital management to arrive on console and begin monitoring the launch preparations. | 
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| L-minus 3 hours, 30 minutes | RF Transmitter Checks | 
	
| The launch team tests the Antares rocket's radio transmitter, which will be the communications link between the vehicle and the ground during flight. | 
	
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| L-minus 3 hours, 30 minutes | Management Call to Stations | 
	
| Orbital management arrives on console in the launch control center. | 
	
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| L-minus 3 hours, 25 minutes | Resume Countdown | 
	
| The countdown resumes after a 15-minute hold. | 
	
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| L-minus 3 hours, 20 minutes | Poll to Initiate LOX Chilldown | 
| The launch team is a polled for a "go" to begin chilldown of the Liquid Oxygen Loading System (LOLS), which conditions the ground and vehicle propellant lines for loading of the cryogenic propellant, which is stored at a temperature of approximately minus 298 degrees Fahrenheit. | 
	
		
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| L-minus 3 hours, 15 minutes | Begin Liquid Oxygen Chilldown | 
| The liquid oxygen chilldown sequence begins. | 
	
		
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| L-minus 2 hours, 48 minutes | FTS Testing | 
	
| The Antares flight termination system, which would destroy the rocket if it flew off course during launch, is tested to ensure it is ready for launch. | 
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| L-minus 2 hours, 24 minutes | Enable Ordnance | 
	
| The Antares rocket's pyrotechnic charges, which are used to separate the rocket's stages and other components in flight, are set to enable. | 
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| L-minus 1 hour, 45 minutes | 15-minute Hold | 
	
| The countdown holds for 15 minutes. | 
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| L-minus 1 hour, 30 minutes | Resume Countdown and Begin Propellant Loading | 
	
| Liquid propellants are pumped into the Antares first stage through the base of the rocket. The 12.8-foot-diameter first stage, fabricated in Ukraine, holds about 21,000 gallons of RP-1 kerosene and about 41,000 gallons of liquid oxygen. The Antares second stage is fueled by solid propellants, which were loaded when the stage was fabricated. | 
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| L-minus 30 minutes | Start of Engine Low-Flow Chilldown | 
	
| The chilldown sequence for the Antares rocket's two AJ26 main engines begins to prepare the engines for ignition. This step narrows the launch window from 15 minutes to 10 minutes. | 
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| L-minus 10 minutes | Start of Engine Medium-Flow Chilldown | 
	
| The chilldown sequence is transitioned to a medium flow. | 
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| L-minus 5 minutes | Transfer Avionics to Internal Power | 
	
| The Antares rocket's avionics are switched to run off of an internal battery. | 
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| L-minus 3 minutes, 30 seconds | Initiate Terminal Countdown | 
	
| The final three-and-a-half minutes of the countdown are run off a computer autosequence. | 
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| L-minus 2 minutes | Pressurize Propellant Tanks | 
	
| The Antares rocket's first stage propellant tanks are pressurized for launch. | 
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| L-minus 15 seconds | Main Engine Slew Test | 
	
| The Antares rocket's AJ26 first stage engines are slewed in a preflight steering check to ensure the gimbal system is ready for flight. The engines can gimbal up to 6 degrees from center to steer the rocket. | 
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| L-minus 5 seconds | TEL Retraction | 
	
| The rocket's umbilical tower, which is also used to transport and erect the vehicle at the launch pad, is retracted away from the launch vehicle. | 
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| L-minus 0 seconds | Main Engine Ignition | 
	
| The two AJ26 main engines ignite with the help of a start cartridge before ramping up to a combined thrust level of approximately 750,000 pounds. | 
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| T+plus 1.5 seconds | Engine Health Check Complete | 
	
| A computer-controlled health check of the performance of the AJ26 engines is completed before liftoff. | 
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| T+plus 2 seconds | Liftoff | 
	
| After the engines are confirmed healthy, the hold-down system releases the Antares rocket at liftoff. | 
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