NEXUS (rocket)

NEXUS heavy-lift booster concept. 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.

Notes

1 2 "Aerospace projects Review". 3 (1).
↑ "SP-4221 The Space Shuttle Decision". NASA History. Retrieved 10 January 2011.

External links

Reusable launch systems

Partially reusable

Active	Falcon 9 Full Thrust

In development	Adeline engine pack for Ariane 6 Baikal booster for Angara Falcon Heavy core stages New Glenn first stage RLV Technology Demonstration Programme Vulcan SMART engine pack

Retired	Buran Space Shuttle

Cancelled	Ares I Ares V Falcon 1e Liquid Fly-back Booster MAKS Phoenix – Hopper Reusable Booster System Saturn-Shuttle

Completely reusable

Active	New Shepard SpaceShipTwo

In development	ITS launch vehicle Skylon SOAR Sura

Retired	SpaceShipOne X-15

Cancelled	Avatar Energia II (Uragan) Goodyear Meteor Junior HOTOL K-1 Lynx Roton SpaceShipThree VentureStar X-30 NASP X-33

Italics indicates suborbital launch systems
‡ - Reusability currently in development

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