Saturn INT-20
The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage. Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five.
Saturn INT-20
The Saturn INT-20 was a proposed intermediate-payload follow-on from the Apollo Saturn V launch vehicle. A conical-form interstage would be fitted on top of the S-IC stage to support the S-IVB stage, so it could be considered either a retrofitted Saturn IB with a more powerful first stage, or a stubby, cut-down Saturn V without the S-II second stage. Three variants were studied, one with three F-1 engines in the first stage, one with four, and one with five.
diameter (μ)
height (mm)
mass (kg)
2304000.0
lower earth orbit payload (kg)
mass (kg)
2304000.0
has abstract
Saturn INT-20 a été une propos ...... moteurs, et une autre à cinq.
@fr
Saturn INT-20 – rakieta nośna ...... ojekt nie został zrealizowany.
@pl
The Saturn INT-20 was a propos ...... with four, and one with five.
@en
country origin
diameter (μ)
height (μ)
lower earth orbit payload (g)
manufacturer
mass (g)
number of rocket stages
status
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Link from a Wikipage to an external page
Wikipage page ID
Wikipage revision ID
712,716,430
alt-diameter
alt-height
alt-mass
5070000.0
alt-stage1thrust
max 7,648,000 lbf
alt-stage2thrust
Caption
INT-20 configuration
stage1engines
stage1fuel
stage1thrust
stage1time
stage2engines
stage2thrust
stage2time
comment
Saturn INT-20 a été une propos ...... moteurs, et une autre à cinq.
@fr
Saturn INT-20 – rakieta nośna ...... ojekt nie został zrealizowany.
@pl
The Saturn INT-20 was a propos ...... with four, and one with five.
@en
label
Saturn INT-20
@en
Saturn INT-20
@fr
Saturn INT-20
@pl
wasDerivedFrom
isPrimaryTopicOf
name
Saturn INT-20
@en