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Simulated view of VentureStar in low Earth orbit, having released its payload
Simulated view of VentureStar in low Earth orbit, having released its payload
VentureStar releases a spacecraft
VentureStar releases a spacecraft
XRS-2200 linear aerospike engine
XRS-2200 linear aerospike engine
The X-33 (left) and VentureStar design (right)
The X-33 (left) and VentureStar design (right)
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The VentureStar was a proposed SSTO spaceplane.
The VentureStar was a proposed SSTO spaceplane.
ROMBUS concept art
ROMBUS concept art
The maiden flight of the DC-X
The maiden flight of the DC-X
Comparison of growth factor sensitivity for Single-Stage-to-Orbit (SSTO) and restricted stage Two-Stage-to-Orbit (TSTO) vehicles. Based on a LEO missi
Comparison of growth factor sensitivity for Single-Stage-to-Orbit (SSTO) and restricted stage Two-Stage-to-Orbit (TSTO) vehicles. Based on a LEO mission of Delta v = 9.1 km/s and payload mass = 4500 kg for range of propellant Isp.