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NEXUS heavy-lift booster concept. Hydrolox truncated plug engine. Atlas ICBM at lower left indicates scale.

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]

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

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This United States-related article is a stub. You can help Wikipedia by expanding it.

[APR-1] "Convair NEXUS". Aerospace Projects Review. 3 (1): 40–80.

[2] "SP-4221 The Space Shuttle Decision". NASA History. Retrieved 10 January 2011.

[Astro-n-3] General Dynamics Nexus - Astronautix

[1]

[2]

[3]

@@ Line 2: / Line 2: @@
 [[Image:NEXUS.jpg|thumb|right|NEXUS heavy-lift booster concept. Hydrolox truncated plug engine. Atlas ICBM at lower left indicates scale.]]
-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.<!--- removed text that was a word for word copy from https://history.nasa.gov/SP-4221/ch2.htm and http://www.astronautix.com/lvs/nexus.htm --> Several versions were designed, including 12,000 and 24,000 [[short ton]] vehicles with payloads of one thousand and two thousand short tons respectively.<ref name="APR">{{cite journal|title=Convair NEXUS |journal=Aerospace projects Review|volume=3|issue=1|pages=40-80 |url=http://www.up-ship.com/eAPR/ev3n1.htm}}</ref> The larger version had a diameter of 202 feet (61.5 metres).<ref name="APR"/><ref>{{cite web|url=https://history.nasa.gov/SP-4221/ch2.htm|title=SP-4221 The Space Shuttle Decision|publisher=NASA History|access-date=10 January 2011}}</ref> It was never built.
+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.<!--- removed text that was a word for word copy from https://history.nasa.gov/SP-4221/ch2.htm and https://web.archive.org/web/20030904131915/http://www.astronautix.com/lvs/nexus.htm --> Several versions were designed, including 12,000 and 24,000 [[short ton]] vehicles with payloads of one thousand and two thousand short tons respectively.<ref name="APR">{{cite journal|title=Convair NEXUS |journal=Aerospace Projects Review|volume=3|issue=1|pages=40–80 |url=http://www.up-ship.com/eAPR/ev3n1.htm}}</ref> The larger version had a diameter of 202 feet (61.5 metres).<ref name="APR"/><ref>{{cite web|url=https://history.nasa.gov/SP-4221/ch2.htm|title=SP-4221 The Space Shuttle Decision|publisher=NASA History|access-date=10 January 2011}}</ref> It was never built.
-It was a [[Single Stage to Orbit]] vehicle that would be fully recoverable upon landing in the ocean.
+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.<ref name=Astro-n>[http://www.astronautix.com/n/nexus.html  General Dynamics Nexus - Astronautix]</ref>
+It would use parachutes to slow descent, with retrorockets (on top) for a final soft touchdown.<ref name=Astro-n>[https://web.archive.org/web/20160825081206/http://www.astronautix.com/n/nexus.html  General Dynamics Nexus - Astronautix]</ref>
 ==Notes==
@@ Line 12: / Line 12: @@
 ==External links==
 *[https://history.nasa.gov/SP-4221/ch2.htm SP-4221 The Space Shuttle Decision - Chapter 2] refs "Astronautics, January 1963, pp. 50-56." re Nexus
-*[http://www.astronautix.com/n/nexus.html Encyclopedia Astronautica - Nexus]
+*[https://web.archive.org/web/20160825081206/http://www.astronautix.com/n/nexus.html Encyclopedia Astronautica - Nexus]
 *[http://www.up-ship.com/eAPR/ev3n1.htm diagrams of NEXUS versions]