MSS Constellation: Difference between revisions
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The '''MSS Constellation''' is a VTHL (vertical take-off and horizontal landing) SSTO (single-stage-to-orbit) reusable launch system designed by [[Javelin Industries]] and [[Dingo Enterprises]]. | |||
[[Category:Spaceships]] | [[Category:Spaceships]] | ||
[[Category:Javelin Industries]] | |||
Latest revision as of 17:54, 13 March 2023
| MSS Constellation. | |
| Type | Reusable single-stage-to-orbit launch vehicle |
|---|---|
| Place of origin |
 Nouvelle Alexandrie Natopia |
| Designed | |
| Manufacturer | Javelin Industries |
| Height | 48.5m |
| Width | 76.5m |
| Payload to low Micras orbit | 45,000 kg |
| Mass | 1,206,500 kg |
| Payload to geostationary transfer orbit | 20,500 kg |
| Stages | 1 or 2 |
The MSS Constellation is a VTHL (vertical take-off and horizontal landing) SSTO (single-stage-to-orbit) reusable launch system designed by Javelin Industries and Dingo Enterprises.
