 | This article or section may need to be cleaned up or summarized because it has been split from/to H-II Transfer Vehicle. |
| Manufacturer | Mitsubishi Heavy Industries |
|---|---|
| Country of origin | Japan |
| Operator | JAXA |
| Applications | ISS resupply |
| Specifications | |
| Spacecraft type | Cargo |
| Launch mass | 16,000 kg (35,000 lb)[1] |
| Payload capacity | Pressurised: 4,070 kg (8,970 lb) Unpressurised: 1,750 kg (3,860 lb)[2] |
| Volume | Pressurised: 78 m3 (2,800 cu ft)[1] |
| Power | 3 kW[1] |
| Design life | |
| Dimensions | |
| Length | 8 m (26 ft) |
| Diameter | 4.4 m (14 ft) |
| Production | |
| Status | In development |
| Maiden launch | 2025 (planned)[3] |
| Related spacecraft | |
| Derived from | H-II Transfer Vehicle |
| Launch vehicle | H3 |
New Space Station Resupply Vehicle (新型宇宙ステーション補給機, Shingata Uchū Sutēshon Hokyūki), tentatively called HTV-X, is an expendable Japanese cargo spacecraft used for International Space Station (ISS) resupply missions. The spacecraft is under development by Japan Aerospace Exploration Agency (JAXA) as the successor of H-II Transfer Vehicle (HTV). As of December 2023[update], the first flight is planned to be launched in early 2025.[3]
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