About: Saturn INT-20   Goto Sponge  NotDistinct  Permalink

An Entity of Type : owl:Thing, within Data Space : platform.yourdatastories.eu:8890 associated with source document(s)

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.

AttributesValues
rdfs:comment
  • 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.
foaf:name
  • Saturn INT-20
foaf:depiction
  • External Image
country origin
diameter (μ)
height (μ)
launch site
lower earth orbit payload (g)
manufacturer
mass (g)
rocket function
number of rocket stages
status
  • Proposal
thumbnail
is successor of
Faceted Search & Find service v1.13.91 as of Nov 14 2017


Alternative Linked Data Documents: ODE     Content Formats:       RDF       ODATA       Microdata      About   
This material is Open Knowledge   W3C Semantic Web Technology [RDF Data]
OpenLink Virtuoso version 07.20.3212 as of Mar 29 2016, on Linux (x86_64-unknown-linux-gnu), Single-Server Edition (68 GB total memory)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2026 OpenLink Software