How are SpaceX's reusable rockets refurbished? What advantages do these systems offer compared to others? What are the technological details behind the cost savings brought by reusability? How do you evaluate this approach?
What does Starship's reusability rely on?
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SpaceX's approach to refurbishing and reflight of Starship hinges on repairing specific components of the rocket using a dedicated system and reintegrating them into the production line. For instance, lower stage heat shields and engine sections, similar to those on the Falcon 9, are retrieved post-landing via helicopter or crane, cleaned, and damaged areas are repaired. The key difference here is Starship's all-steel construction, which simplifies the maintenance process. Typically, rockets are discarded after a single use, but with Starship, only components like bushings, valves, or certain engine parts are replaced. You can think of it like changing the oil in a car, albeit with much more advanced technology.
When comparing these aspects to the Falcon 9, significant differences emerge. While the Falcon 9's lower stage costs around $2.8 million, SpaceX's calculations show that Starship's full reusability can reduce the total cost by up to 90%. Looking at other systems, such as Blue Origin's New Glenn, which is also designed for reusability, it lacks Starship's all-metal, single-piece design, making maintenance more complex. In essence, SpaceX's approach treats the entire rocket like a ship, sending it to the "mechanic" for maintenance after each flight, whereas others can only refurbish specific parts. This ultimately drives down the flight cost in the long run to nearly the cost of the rocket's raw materials.
Starship's reusability is one of SpaceX's biggest advantages, but it comes with serious engineering behind it. I think the most important detail is that every part of the rocket is designed modularly and can be easily replaced. For example, Starship uses 3D-printed custom tiles for its thermal protection system (TPS) in the lower section, and each one can be swapped out for a new one with ease. Funny enough, I actually use a similar approach in Figma—when building design systems, creating reusable components boosts efficiency.
From a cost perspective, as the number of reuses increases, launch costs have dropped by nearly 90%. This gives SpaceX an edge in projects like Starlink. What I admire most about SpaceX's approach is that they don’t just refurbish engines—they design the entire rocket to require minimal maintenance. For instance, Raptor engines' fuel pumps and combustion chambers only need cleaning after their first use; there’s no need to fully disassemble and replace them.
Starship's reusability system is actually built on four main components: the heat shield, engines, landing systems, and overall engineering design. For the heat shield, SpaceX uses a material called **PICA-X**, which can withstand temperatures up to 2,700°C during atmospheric entry and has a long lifespan. The engines, the **Raptor** engines, are designed to be super durable and easy to retest. For example, before reusing the engines, they heat them up to just 1,000°C to minimize corrosion and damage.
Honestly, even for frontend devs like me, the logic is simple: a reusable rocket only recovers the cost of fuel—which is astronomical—and the initial construction. Unlike other companies, SpaceX can recover almost the entire rocket, including the upper stage Starship. This eliminates millions of dollars in costs per launch. To me, the most interesting part is this "rapid reuse" culture—they treat rockets almost like airplanes, able to relaunch them within hours after maintenance. Other methods either only recover boosters (like Blue Origin) or scrap the entire system after a few flights. SpaceX is in a completely different paradigm. I think this approach could even change the path to Mars, honestly.
Starship's reusability is primarily based on its Thermal Protection System (TPS) and integrated body design. This system, called RHS (Reusable Heat Shield), consists of nearly 30,000 heat shields that protect both the body and from extreme heat during flight. These shields are made of ceramic fiber coated with SpaceX's proprietary "6061 aluminum-steel intermetallic" alloy, which melts to provide protection when overheated to a superheated state. One of the most critical aspects for reuse is the heat flux (~1200°C) the modules are exposed to during landing, against which advanced "active cooling" and "ablative spraying" technologies are employed.
Unlike other rockets (e.g., NASA's Space Shuttle), Starship offers a fully reusable system, including the upper stage. In the Shuttle, only the main engines (SSME) and solid rocket boosters (SRB) could be partially recovered; whereas in Starship, both the body and the booster (Super Heavy) can be recovered. This is expected to reduce launch costs by more than tenfold, focusing on "mass cleaning/repair processes" rather than "individual component refurbishment." The cost advantage from reusability stems from the standardization of the "booster refurbishment process": SpaceX aims to have a Starship ready for flight within 90 days through fully autonomous landing and launch operations—compared to the Shuttle program, where this process took 100+ days.