MSS Constellation: Difference between revisions
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{{Nouvelle Alexandrie Article}} {{Natopian article}} | |||
{{ infobox | {{ infobox | ||
| bodyclass = toccolours | | bodyclass = toccolours | ||
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| data2 = Reusable single-stage-to-orbit launch vehicle | | data2 = Reusable single-stage-to-orbit launch vehicle | ||
| label3 = Place of origin | | label3 = Place of origin | ||
| data3 = {{team flag|Nouvelle Alexandrie}} | | data3 = {{team flag|Nouvelle Alexandrie}}<br>{{team flag|Natopia}} | ||
| label4 = Designed | | label4 = Designed | ||
| data4 = {{Unbulleted list|[[Javelin Industries]]|[[Dingo Enterprises]]}} | | data4 = {{Unbulleted list|[[Javelin Industries]]|[[Dingo Enterprises]]}} | ||
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| data11 = 1 or 2 | | data11 = 1 or 2 | ||
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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]] | [[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.