The NEXUS reusable rocket was a concept design created in the 1960s by a group at General Dynamics led by Krafft Arnold Ehricke. It was intended as the next leap beyond the Saturn V, carrying up to eight times more payload. Several versions were designed, including 12,000 and 24,000 short ton vehicles with payloads of one thousand and two thousand short tons respectively.[1] The larger version had a diameter of 202 feet (61.5 metres).[1][2] It was never built.
It was a single-stage-to-orbit vehicle that would be fully recoverable upon landing in the ocean. It would use parachutes to slow descent, with retrorockets (on top) for a final soft touchdown.[3]
YouTube Encyclopedic
-
1/3Views:196 88714 699 2882 286 916
-
Convair Nexus Reusable SSTO Rocket: Proposed Saturn V Replacement
-
World's first passenger drone Ehang 184 delivers holiday gifts
-
Flying an $80 000 MICRO ARMY FPV DRONE!!!!!!!!
Transcription
Notes
- ^ a b "Convair NEXUS". Aerospace Projects Review. 3 (1): 40–80.
- ^ "SP-4221 The Space Shuttle Decision". NASA History. Retrieved 10 January 2011.
- ^ General Dynamics Nexus - Astronautix
External links
- SP-4221 The Space Shuttle Decision - Chapter 2 refs "Astronautics, January 1963, pp. 50-56." re Nexus
- Encyclopedia Astronautica - Nexus
- diagrams of NEXUS versions
 | This rocketry article is a stub. You can help Wikipedia by expanding it. |
 | This United States–related article is a stub. You can help Wikipedia by expanding it. |
This page was last edited on 31 March 2023, at 15:35