The block logic
Each Block Is a Redesign, Not a Trim
Falcon evolved in place over a decade. Starship changes generation about once a year, and each one reworks tanks, engines and control surfaces together.
A block is a coordinated redesign of both stages, flown as a batch and then retired whole. Block 1 proved the stack could fly and be caught. Block 2 stretched the tanks and reshaped the flaps but never reached its payload goal. Block 3, flying since May 2026, is the first built around Raptor 3, refueling hardware and the grid-fin catch. Block 4, planned for 2027, stretches the whole vehicle and adds engines to the ship. The through-line is the same across all four: the airframe kept gaining mass as heat shield, reinforcement and reuse hardware were added, so SpaceX stopped chasing weight down and scaled the vehicle up instead.
The pattern that matters for everything downstream: payload to low Earth orbit went from 15 t on Block 1 to a planned 200 t on Block 4, an order of magnitude in four generations, while the diameter never moved off 9 m. The growth came from taller tanks, denser engines and lighter structure, not a wider vehicle. Building
Stack at a glance
The Whole Vehicle, Block by Block
Integrated figures for the full stack. Booster and ship detail follow in their own sections.
| Measure | Block 1 | Block 2 | Block 3 | Block 4 |
|---|---|---|---|---|
| Stack height | 121.3 m | 123.1 m | 124.4 m | ~142 m est. |
| Diameter | 9 m | 9 m | 9 m | 9 m |
| Payload to LEO | 15 t | 35 t | 100 t | ~200 t est. |
| Engines, total | 33 + 6 | 33 + 6 | 33 + 6 | 33 + 9 |
| First flight | Apr 2023 | Jan 2025 | May 2026 | 2027 planned |
| Status | Retired | Retired | Flying | Planned |
| Flights flown | 6 | 5 | 2 | 0 |
Block 2’s 35 t is the figure it retired at. Its original target was at least 100 t; the ship never flew an orbital mission before it was retired after Flight 11. Block 4 height, payload and mass are SpaceX estimates, not flown numbers.
Super Heavy by block
The Booster: Same 33 Engines, a Deeper Redesign Underneath
Engine count held at 33 through Block 3. What changed was the interstage, the grid fins, the shielding and the engine generation.
| Measure | Block 1 & 2 | Block 3 | Block 4 |
|---|---|---|---|
| Height | 71 m | 72.3 m | ~81 m est. |
| Propellant | 3,250–3,400 t | 3,650 t | 4,050 t planned |
| Engines | 33 × Raptor 2 | 33 × Raptor 3 | 33 × Raptor 3/4 |
| Liftoff thrust | 73.5 MN | 80.8 MN | ~98 MN planned |
| Grid fins | 4, upper | 3, larger, lower | 3 |
| Interstage | Vented, jettisoned (B11 on) | Integrated, retained | Integrated |
| Relight for boostback | Inner 13 only | All 33 | All 33 |
Three Block 3 changes carry most of the weight. The interstage folds into the methane tank instead of being a separate vented ring that was thrown away in flight, which removes a jettison event. The grid fins drop from four to three, grow about half again in size, sit lower on the vehicle, and now serve as the tower catch points — so the separate catch hardware the earlier boosters carried is gone. And because Raptor 3 moves its own plumbing inside the engine, most of the engine-bay shielding comes off, saving over a tonne per engine. All 33 Block 3 engines can relight, where Block 1 and 2 could only relight the inner 13 for boostback.
Ship by block
The Ship: Where the Flaps, Tiles and Refueling Hardware Changed
The upper stage is also the spacecraft, so its blocks carry the heat shield, the flaps and, from Block 3, the docking gear for orbital refueling.
| Measure | Block 1 | Block 2 | Block 3 | Block 4 |
|---|---|---|---|---|
| Height | 50.3 m | 52.1 m | ~52 m | ~61 m est. |
| Propellant | 1,200 t | 1,500 t | 1,600 t | 2,300 t planned |
| Engines | 3 SL + 3 vac | 3 SL + 3 vac | 3 SL + 3 vac | 3 SL + 6 vac |
| Forward flaps | Larger, 180° | Thinner, leeward, ~140° | As Block 2 | As Block 2 |
| Engine type | Raptor 2 | Raptor 2 (upgraded) | Raptor 3 | Raptor 3/4 |
| Refueling hardware | None | None | Docking port, new QD | Docking port |
| Result | Retired after Flight 6 | Retired after Flight 11 | Flying | Planned |
Block 2’s signature change was the forward flaps: moved leeward, made thinner, and set at roughly 140° instead of 180°, after Block 1 ships took repeated flap burn-through on reentry — near-total loss on Flight 4. Block 3 keeps that flap geometry and adds what the beyond-LEO mission needs: docking ports and a redesigned quick disconnect for ship-to-ship refueling, plus a revised tile design. The Block 3 ship also carries a “crunch wrap” felt between tiles, added after Flight 10, to stop heat seeping through the gaps. Block 4 adds three more Raptor Vacuum engines, taking the ship from six engines to nine.
Raptor generations
The Engine Generation Sets the Block
Full-flow staged combustion on subcooled methalox throughout. Each Raptor generation removes external hardware and raises thrust.
| Generation | Thrust, sea level | Flew on | Rated |
|---|---|---|---|
| Raptor 1 | ~185 tf | Early hop prototypes; never an integrated flight test | Observed |
| Raptor 2 | ~230 tf | Flights 1–11, all Block 1 and Block 2 | Observed |
| Raptor 3 | ~280 tf | Block 3, from Flight 12. Plumbing and sensors internal, so no separate engine heat shield | Observed |
| Raptor 4 | ~300 tf target | Planned for Block 4; not yet flown or confirmed in detail | Modeled |
The jump that changed the airframe was Raptor 3. By internalizing the plumbing it let SpaceX strip the engine-bay shielding from both stages — the single biggest reason a Block 3 vehicle looks cleaner around the engines than a Block 2 one. Full engine detail lives on the Raptor page.
Grid fins and catch
Four Fins Became Three, and the Fins Became the Catch Point
The most visible Block 3 change is also a recovery change: the booster no longer carries dedicated catch hardware.
Block 1 and 2 boosters had four grid fins near the top of the vehicle and separate protruding hardpoints for the tower arms to grab. Block 3 goes to three larger fins in a 90/90/180 arrangement, set lower on the booster, with the catch pins integrated into the fins themselves. SpaceX says the lower position reduces the heat the fins take during stage separation. Removing the separate catch structure saves mass, but it also means the fin and the catch point are now one part — a fin failure and a catch failure are no longer independent.
This is why no Block 3 booster has yet been caught: the three catches on record — Boosters 12, 14 and 15, from October 2024 on — were all Block 1 and Block 2 vehicles with the four-fin, separate-hardpoint layout. The Block 3 catch is unproven, and it is the recovery milestone Flight 15 may attempt. Recovery in full is on the hub’s recovery section.
Retirement sequence
Blocks Retire Whole, on the Flight That Ends Them
SpaceX does not phase blocks together. A generation flies its batch and stops on a named flight.
| Block | Span | Last flight & outcome | Rated |
|---|---|---|---|
| Block 1 | Flights 1–6, 2023–24 | Retired after Flight 6 (Nov 2024). Four successes, first tower catch on Flight 5 | Observed |
| Block 2 | Flights 7–11, 2025 | Retired after Flight 11 (Oct 2025). Three ship failures early; last two flights reached target. Also the last flights from Pad 1 before its rebuild | Observed |
| Block 3 | Flight 12 onward, 2026– | Flying. Both flights so far reached ship targets; neither booster survived landing | Building |
| Block 4 | 2027 planned | Needs the Gigabay integration buildings to stack the stretched vehicle | Projected |
Booster 18, the first intended Block 3 booster, was scrapped after test damage, so Block 3 debuted on Booster 19. That is why the first Block 3 flight is Flight 12 rather than an earlier number, and why the booster and ship serial numbers no longer track the flight number.
Contested
Deliberately Not Claimed
The load-bearing uncertainties, tagged with the confidence they actually earn.
Every Block 4 figure is an estimate. Height near 142 m, about 200 t to LEO, a nine-engine ship and a booster near 98 MN come from SpaceX statements and reporting, not flown hardware. The engine total for Block 4 is sometimes quoted as 42 (33 booster plus 9 ship). Treat the whole column as a target.
Block 3 booster thrust is quoted in a range. Sources give 80.8 MN for the block specifically and a higher integrated figure in some summary tables. This page uses the block-specific 80.8 MN. The higher numbers appear tied to later Raptor 3 variants or Block 4 assumptions.
Block 2 never met its payload goal. It was announced at 100 t or more to orbit and retired at an estimated 35 t, having never flown an orbital mission. The gap is not a measurement dispute — the vehicle was replaced before it flew the mission that would have tested the claim.
Record
Provenance and Data Sources
- Confidence
- Observed for flown blocks and their measured figures — Building for Block 3 in progress — Projected for Block 4 estimates — Modeled for unflown engine variants
- Status date
- Q3 2026, ahead of Flight 14
- Vehicle figures
- SpaceX Starship and Super Heavy technical records; SpaceX Starship update (April 2024) introducing Block 2 and Block 3
- Engines
- Raptor generation figures from McGregor test observations and SpaceX statements
- Flights
- Flight records for Flights 1 through 13; block retirement points at Flights 6 and 11
- Block 4
- SpaceX estimates and reporting; not flown
- Weakest link
- The entire Block 4 column, and Block 3 booster landing, not yet demonstrated