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The global launch market reached $14.1 billion in 2024 — up 34% since 2021.
| Attribute | |||
|---|---|---|---|
| Company | SpaceX | Khrunichev / Roscosmos | ULA |
| Country | 🇺🇸 USA | 🇷🇺 Russia | 🇺🇸 USA |
| Status | Active | Active | Active |
| Vehicle class | Medium | Heavy | Heavy |
| Propellant | RP-1 / LOX | RP-1 / LOX (RD-191, all 5 modules) | LNG / LOX (BE-4); LH₂ / LOX (Centaur V) |
| Reusable | Yes | No | No |
| Stages | 2 | 2 | 2 |
| First flight | 2010 | 2014 | 2024 |
| Payload to LEO | 22,800 kgas of [1]Reusable first stage (expended gives 22,800 kg; reused gives ~15,600 kg) | 24,500 kgas of [1]With KVTK cryogenic upper stage (planned); Briz-M gives ~5,400 kg GTO | 27,200 kgas of [1]VC2S configuration (2 solid strap-on boosters) ↑ Best |
| Payload to GTO | 8,300 kgas of [1]Expendable configuration. Reusable GTO capacity ~5,500 kg. | 5,400 kgas of [1]Briz-M upper stage. KVTK would raise this to ~7,500 kg. | 14,400 kgas of [1] ↑ Best |
| Height | 70 mas of [1] ↑ Best | 64 mas of [1] | 61.6 mas of [1] |
| Liftoff mass | 549 tas of [1] | 773 tas of [1] ↑ Best | 591 tas of [1]VC2S configuration |
| Success rate | 99.5%as of [2]634/637 full successes; Block 5 alone 580/581 = 99.8% | 100%as of [2]4/4 mission successes: Dec 2014, Dec 2020, Mar 2023, Apr 2024 ↑ Best | 100%as of [2]4/4 mission successes: VC2 Cert-1 (Jan 2024), VC2 Cert-2 (Oct 2024), VC4 USSF-87 (Feb 2026), VC2 USSF-106 (Mar 2026) ↑ Best |
| Total flights | 637as of [2] ↑ Best | 4as of [2] | 4as of [2] |
| Cost / kg LEO | ~$2,720/kgas of [1]Based on $67M list price / 22,800 kg LEO (expendable) ↓ Cheapest | — | ~$5,500/kgas of [1]Estimated; list pricing not public. Priced below Atlas V, above Ariane 6. |
| Summary | The world's most frequently flown orbital rocket. Block 5 first stages have landed over 280 times and reflown up to 23 times. Backbone of Starlink and commercial crewed launches. | Russia's new-generation heavy-lift rocket built entirely of Russian-manufactured components — a political priority after Proton-M's dependence on Ukrainian components. Five URM-1 universal rocket modules share the same propellant (RP-1/LOX), unlike Proton-M's toxic hypergolics. Flight rate remains very low. | ULA's next-generation medium-heavy rocket replacing Atlas V. Powered by two BE-4 engines on the first stage and a cryogenic Centaur V upper stage. Primary customer is USSF under NSSL Phase 2. |
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.