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Subject Item
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Saturn-Shuttle
rdfs:comment
The Saturn-Shuttle was a preliminary concept of launching the Space Shuttle orbiter using the Saturn V rocket. An interstage would be fitted on top of the S-IC stage to support the external tank in the space occupied by the S-II stage in the Saturn V, so that NASA would have been able to steer completely away from solid rockets.
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n14:
n15: n39:
n34:
10 m
n29:
475.0
n32:
212.0
n36:
concept was studied in 1972
n9:
or
n12:
Saturn-Shuttle
n42:
281.0
n24:
NASA model of Saturn-Shuttle configuration
n22:
Manned LEO launch vehicle
n5:
United States
n50:
Shuttle Orbiter & External Tank
n43:
max 60,500 kg
n30:
n31:
n6:
2304000.0
n37:
2
n40:
85 m
n21:
Rockwell International Boeing Martin Marietta
n52:
33.0
n38:
max 7,648,000 lbf
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max 34.02 MN
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133400.0
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5070000.0
n33:
3
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5
n45:abstract
The Saturn-Shuttle was a preliminary concept of launching the Space Shuttle orbiter using the Saturn V rocket. An interstage would be fitted on top of the S-IC stage to support the external tank in the space occupied by the S-II stage in the Saturn V, so that NASA would have been able to steer completely away from solid rockets. The addition of wings on the S-IC stage would allow the booster to fly back to the Kennedy Space Center, where technicians would then refurbish the booster (by replacing only the five F-1 engines and reusing the tanks and other hardware for later flights).}}[citation needed] The Shuttle would handle space station logistics, while Saturn V would launch components. This would have allowed the International Space Station, using a Skylab or Mir configuration with both U.S. and Russian docking ports, to have been lifted with just a handful of launches. The Saturn-Shuttle concept also would have eliminated the Space shuttle solid rocket boosters that ultimately precipitated the Space Shuttle Challenger accident in 1986.