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 | NASA / Boeing | CASC / SAST | Khrunichev / Roscosmos |
| Country | 🇺🇸 USA | 🇨🇳 China | 🇷🇺 Russia |
| Status | Active | Active | Retired |
| Vehicle class | Super Heavy | Medium | Heavy |
| Propellant | LH₂ / LOX (RS-25); solid HTPB (SRBs) | UDMH / N₂O₄ (hypergolic all stages) | UDMH / N₂O₄ (hypergolic — all stages) |
| Reusable | No | No | No |
| Stages | 2 | 2 | 3 |
| First flight | 2022 | 1992 | 2001 – 2023 |
| Payload to LEO | 95,000 kgas of [1] ↑ Best | 3,500 kgas of [1]SSO capacity ~1,300 kg; standard LEO 3,500 kg | 22,400 kgas of [1] |
| Payload to GTO | 27,000 kgas of [1]Trans-lunar injection (TLI) payload; GTO not a primary design goal ↑ Best | — | 6,290 kgas of [1]With Briz-M upper stage |
| Height | 98.1 mas of [1] ↑ Best | 41.06 mas of [1] | 58.2 mas of [1] |
| Liftoff mass | 2,608 tas of [1] ↑ Best | 232 tas of [1] | 712 tas of [1] |
| Success rate | 100%as of [2]2/2: Artemis I uncrewed (Nov 16, 2022) + Artemis II crewed lunar flyby (Apr 1–10, 2026) ↑ Best | 98.7%as of [2]~77/78 successes; one known failure (CZ-2D Y7, Mar 1995 upper-stage anomaly) | ~91%as of [2]~13 mission failures out of ~115 flights in Proton-M variant; highly toxic propellant complicated recovery operations |
| Total flights | 2as of [2] | ~78as of [2] | ~115as of [2]Effectively retired ~2023 with Russian government replacing it with Angara A5 ↑ Best |
| Cost / kg LEO | ~$40,000+/kgas of [3]NASA OIG (2023) estimated $4.1B per Artemis SLS/Orion flight; total program $23B+ development cost ↓ Cheapest | — | — |
| Summary | NASA's human deep space launch vehicle for the Artemis programme. Uses heritage RS-25 shuttle main engines (4 per flight, expended). Block 1B with Exploration Upper Stage cancelled Feb 2026; Block 1 will fly through Artemis IV at minimum. | China's most-used sun-synchronous and polar orbit workhorse for small-to-medium military and commercial Earth observation satellites. Launched from Jiuquan and Taiyuan. Uses storable hypergolic propellants for high launch-readiness but produces toxic exhaust. | Russia's dominant heavy-lift rocket for GEO comsats and planetary missions from 1965 (Proton family) through 2023 (Proton-M). Notorious for its hypergolic propellant — a highly toxic UDMH/N₂O₄ combination that caused environmental concerns at Baikonur. Replaced by Angara A5. |
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.