Pick up to 4 launch vehicles to compare side-by-side. State lives in the URL — share the link and the comparison loads exactly as you left it.
The global launch market reached $14.1 billion in 2024 — up 34% since 2021.
| Attribute | |||
|---|---|---|---|
| Company | SpaceX | JAXA / Mitsubishi Heavy Industries | Roscosmos / Progress Rocket Space Centre |
| Country | 🇺🇸 USA | 🇯🇵 Japan | 🇷🇺 Russia |
| Status | In Development | Active | Active |
| Vehicle class | Super Heavy | Heavy | Medium |
| Propellant | CH₄ / LOX | LH₂ / LOX (LE-9 first stage + LE-5B-3 second stage) | RP-1 / LOX |
| Reusable | Yes | No | No |
| Stages | 2 | 2 | 3 |
| First flight | 2023 | 2024 | 2004 |
| Payload to LEO | ~150,000 kgas of [1]SpaceX projected max payload in fully expendable mode; ~100,000 kg reusable ↑ Best | 16,500 kgas of [1]H3-24 (2 SRB-3 + 4 LE-9 engines) configuration. H3-30 baseline: 16,500 kg. | 8,200 kgas of [1]Soyuz-2.1b with Fregat upper stage; 2.1a variant ~7,020 kg LEO |
| Payload to GTO | ~21,000 kgas of [1]Reusable configuration estimate ↑ Best | 6,500 kgas of [1] | 3,250 kgas of [1]With Fregat-M upper stage |
| Height | 121 mas of [1]Version 2 (V2) full stack Ship + Super Heavy ↑ Best | 57 mas of [1] | 46.3 mas of [1] |
| Liftoff mass | ~5,000 tas of [1] ↑ Best | 574 tas of [1]H3-24S configuration | 312 tas of [1] |
| Success rate | ~55%as of [2]IFT-1 through IFT-11; ~6 complete mission successes, remainder partial or vehicle lost. No orbital payload deployment yet. | 75%as of [2]~6/8 successes. TF1 (Feb 2023) first flight failure (LE-9 ignition issue, DAICHI-3 lost). F8 (Dec 23, 2025) QZS-5 lost to 2nd-stage relight anomaly. | 97%as of [2]~160/165 mission successes since 2004 per aggregated launch logs ↑ Best |
| Total flights | 11as of [2]IFT-1 (Apr 2023) through IFT-11 (May 2026 target). IFT-10 (Aug 2025) achieved full mission: booster caught + Ship splash-down. | 8as of [2] | ~165as of [2] ↑ Best |
| Cost / kg LEO | ~$600/kgas of [1]SpaceX target figure; not yet achieved in operational configuration ↓ Cheapest | ~$5,500/kgas of [1]Target unit price ¥5B (~$35M at ¥145/$); roughly half H-IIA's per-launch cost | — |
| Summary | Largest and most powerful rocket ever flown. Super Heavy booster uses 33 Raptor engines. V3 Ship introduced Aug 2025. Mechazilla caught the booster on IFT-5 (Oct 2024) and IFT-10 (Aug 2025). Primary vehicle for Artemis HLS lunar landing (Artemis III planned 2026). | Japan's next-generation flagship rocket designed to halve H-IIA costs. Uses three LE-9 engines burning liquid hydrogen — the highest-performing expander-cycle engines in the world. First successful flight was TF2 (Feb 17, 2024). HTV-X1 cargo mission to ISS (Oct 2025) demonstrated operational readiness. | Russia's primary medium-lift workhorse, descended from the Soyuz family that has flown since 1966. Carries both crewed Soyuz spacecraft and Cygnus-class cargo. Fregat upper stage significantly expands mission flexibility. Production continues at Samara (now TsSKB-Progress). |
28 launch vehicles across 10 countries — active, retired, and in development — with primary-source citations from manufacturer user guides and agency press kits. Pure URL state: bookmark or share the link and the comparison reproduces exactly.