SpaceX’s CRS-18 Dragon spacecraft has concluded her EOM (End Of Mission) milestones, following unberthing from the International Space Station (ISS) on Tuesday. Dragon’s release from the Space Station Remote Manipulator System (SSRMS) occurred at 14:59 UTC, with splashdown in the Pacific Ocean around 20:20 UTC.
The CRS-18 Dragon was launched on Falcon 9 B1056.2 last month. This was the same booster that had also launched the CRS-17 Dragon.
Once again, the booster made a successful return and will be prepared for a future launch.
Dragon delivered over 2,500kg of cargo in her pressurized, including food and consumables for the ISS crew and several major scientific investigations set to be carried out in the space station’s microgravity environment.
One of the largest pieces of equipment is the third International Docking Adapter (IDA-3), which was lofted in the Dragon’s unpressurized “trunk” and removed during docked ops.
This was recently installed to Pressurized Mating Adapter-3 on the space-facing side of the station’s Harmony module during EVA-55.
Ahead of the return trip, Dragon was packed with downmass and the hatch closed. Dragon will be returning almost 2,700 pounds of scientific experiments and other cargo as downmass, including some numerous samples.
Robotic ground controllers then used the robotic arm to detach Dragon from the Earth-facing port of the Harmony module to maneuver Dragon into the release position.
Dragon was unberthed by the Space Station Remote Manipulator System (SSRMS) before being released from the robotic arm at 14:59 UTC. This was slightly later than planned due to the requirement to gain better lighting conditions.
Once the LEE snares were released, the SSRMS was backed away from Dragon as the craft held its position at the 10-meter mark.
Once the Station’s arm was cleared to a safe distance, Dragon conducted a series of three small thruster firing departure burns that moves the capsule down the R-Bar (Radial Vector) and away from the International Space Station toward Earth (when viewed in relation to ISS orientation and Dragon movements with respect to Earth).
During the initial stage of departure, Dragon was under the control of its own computer programming, with the Station crew and controllers at Mission Control Houston in Texas for NASA having primary control over the spacecraft.
As Dragon pushed down the R-Bar, the largest of the three thruster departure burns imparted enough Delta Velocity (Delta-V) change to Dragon to push it outside of the approach ellipsoid.
The approach ellipsoid is a 4 km by 2 km oval-shaped region around the International Space Station that extends 2 km in front of and 2 kilometers behind the ISS along the velocity vector (V-Bar) and 1 km above and 1 km below the Station along the R-Bar.
Once Dragon cleared the approach ellipsoid 1 km below the ISS, primary control of the vehicle shifted from NASA to SpaceX controllers in Hawthorne, California.
Dragon conducted several hours of free flight activities as controllers at Mission Control SpaceX prepared the vehicle for the end of its mission.
This included the closure of the Guidance Navigation and Control (GNC) bay door on Dragon, creating a perfect thermal protection seal around the entirety of Dragon for entry.
SpaceX flight controllers at Hawthorne, California commanded Dragon’s Draco thrusters to fire for 12 minutes and 53 seconds – retrograde – in the deorbit burn. This enabled Dragon to slip out of orbit for its descent back to Earth.
Following the deorbit burn, the umbilicals between Dragon and her external payload trunk were severed ahead of the trunk’s separation from Dragon itself.
Dragon then placed its heat shield out in front in preparation for Entry Interface (EI) – the moment Dragon reached the first traces of Earth’s upper atmosphere.
Once EI occurred, Dragon’s Thermal Protection System (TPS) protected it from the searing hot temperatures of reentry formed as the air molecules around Dragon are instantly heated and turned to plasma under the friction created by Dragon’s high velocity.
Dragon’s primary heat shield, called PICA-X, is based on a proprietary variant of NASA’s Phenolic Impregnated Carbon Ablator (PICA) material and is designed to protect Dragon during atmospheric re-entry.
PICA-X is robust enough to protect Dragon not only during ISS return missions but also during high-velocity returns from Lunar and Martian destinations. There were also signs of some experimental tiles on the Dragon that are understood to be related to SpaceX’s Starship test program.
Unlike the Dragon capsule, the Dragon trunk destructively burns up in Earth’s atmosphere.
Once safely through the plasma stage of reentry, Dragon’s drogue parachutes deployed, followed by the main chutes designed to ease the vehicle to a splashdown in the Pacific Ocean for recovery.
Recovery is attained by three main recovery vessels which were positioned near Dragon’s return location. The main recovery vehicle had already set sail earlier in the last few days.
Fast recovery vessels deploy, collecting Dragon’s parachutes as the recovery of the capsule itself is conducted by the primary recovery assets.
Dragon’s parachute-assisted splashdown usually occurs 410 miles southwest of Long Beach, California.
It will take about two days for Dragon to be brought back to the Port of Los Angeles for its cache of cargo and scientific experiments to be unloaded.
The ISS crew spent the majority of the second half of Dragon’s stay loading Dragon’s pressurized capsule with key items to be returned to Earth, including numerous time-sensitive experiments, which will be the first items to be removed.
Dragon will eventually take a road trip to SpaceX’s test center at McGregor in Texas for the complete cargo removal.