Starlink Group 4-34 mission to complete SpaceX doubleheader


A SpaceX Falcon 9 Block 5 carrying 54 Starlink satellites is targeted to launch at 10:10 PM EDT on September 13 (02:10 UTC on September 14). This mission will be launching from Space Launch Complex 40 (SLC-40) at the Cape Canaveral Space Force Station in Florida.

The booster supporting Starlink Group 4-34 is B1067, which has flown on five previous missions. B1067 debuted on the CRS-22 mission and went on to launch the Crew-3, Turksat-5B, Crew-4, and CRS-25 flights.

To initialize the automated launch sequence at T-38 minutes, SpaceX’s Launch Director gives the “go” for propellant loading. At T-35 minutes, sub-cooled RP-1 kerosene will be loaded into both the first and second stages, and the first stage will also begin being loaded with liquid oxygen (LOX).

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At T-20 minutes, the RP-1 loading into the second stage will be complete, and a large vent from the Transport Erector (T/E) can be seen. This is to purge the T/E’s lines of RP-1 in preparation for the second stage’s next phase of fueling: at T-16 minutes, LOX will begin being loaded into the second stage. Once LOX loading is completed, RP-1 on the first stage and LOX on both stages will be topped off until T-90 seconds.

The next milestone of the launch sequence occurs at T-7 minutes, at which point the Falcon 9 first stage begins engine chill—the booster flows a small amount of LOX through the oxygen section of each M1D turbo pump, preventing propellant from flashing into a gas at engine ignition, which could severely damage the engine.

Next, at T-1 minute, the flight computer takes over the countdown in what is called “startup” and begins the final prelaunch checks. At the same time, the propellant tanks will pressurize to match the pressures required during the flight. Once this is completed, a call out of “tanks are pressed for flight” can be heard.

The T-20 minute vent before the launch of Nilesat-301 in June 2022. (Credit: Stephen Marr for NSF)

Next, the Launch Director will verify the final “go” for launch at T-45 seconds. Then at T-3 seconds, the engine controller sends the command for ignition of the first stage’s nine Merlin 1D engines. By T-0.02 seconds, the engines and vehicle will be running independently and be ready for flight, and the vehicle will command the hydraulic launch clamps to release at T0, allowing the vehicle to liftoff.

Following liftoff, the vehicle will encounter Max-Q – the moment of maximum aerodynamic pressure – at T+1 minute and 12 seconds. The first stage Merlin 1D engines will remain lit until T+2 minutes and 27 seconds, at which point a series of events occur in quick succession. First, all nine M1D engines will shut down, followed shortly after by the separation of the stages. The second stage will then ignite its single M1D Vacuum engine.

The fairings, which protect the payloads from debris and atmospheric heating during ascent, will separate from the vehicle at T+3:13. Both fairing halves utilize RCS thrusters and parachutes to re-enter the atmosphere and softly splashdown in the Atlantic Ocean. The fairing halves will then be recovered by SpaceX’s fairing recovery ship, Doug.

Also following stage separation, the first stage will deploy its four grid fins and perform a series of thruster maneuvers to properly orientate itself for re-entry into Earth’s atmosphere. At T+7:07, the first stage’s re-entry burn begins and will continue for the next 31 seconds. The first stage will then coast back toward Earth, continuing to use its grid fins to orient itself for an on-target landing.

Falcon 9 B1052 in Port Canaveral onboard JRTI after the KPLO mission in August 2022. (Credit: Julia Bergeron for NSF)

At T+8:26, the first stage will initiate a third burn to slow itself down for a soft landing on SpaceX’s Autonomous Spaceport Drone Ship (ASDS) Just Read the Instructions (JRTI) off the coast of North Carolina.

Once the second stage reaches its desired parking orbit, Second Engine Cut Off (SECO) will occur and the stage will briefly coast in preparation for payload deployment.

The second stage then begins to rotate over its x-axis, before deploying the four tension rods at T+15 minutes and 21 seconds. Due to the stage’s rotation, the 54 Starlink satellites will have varying amounts of angular momentum, causing them to separate once the tension rods are deployed.

The Starlink satellites will now spend the following months raising their orbit to Starlink Shell 4: a 540 km circular orbit at 53.2 degrees inclination. SpaceX has at least two more missions in September, including at least one more Starlink mission and the Transport and Tracking Layer (TTL) Tranche 0 Flight 1 mission for the Space Development Agency (SDA).

(Lead photo: Falcon 9 B1051 at SLC-40 before the launch of Starlink v1.0 L3 in January 2020. Credit: Stephen Marr for NSF)

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