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The Saturn V thread - NASASpaceFlight.com 27 Jan 2006 · The Saturn V threadDifferent beasts and as such people don't like to compare. But the full Saturn V, remember there were more versions, was 7.5 million lbs thrust from liquid …
Saturn V staging 28 Feb 2009 · ugordon's animated avatar of a Saturn V staging is quite interesting, but I wanted some confirmation of what I am seeing. 1. The center engine on the S-1C appears to have …
We Can’t Rebuild Saturn V, But… 18 Mar 2025 · If NASA wanted to replicate Saturn V, then they could use a Superheavy booster from SpaceX, and upper stages made from BE-3U Blue Origin engines. A cluster of 10-12 on a …
Saturn V 1st and 2nd stage splashdown - NASASpaceFlight.com 5 Aug 2007 · Saturn V 1st and 2nd stage splashdownThe S-IC was tail-heavy and settled into a re-entry from high speed/high altitude engines-first. Aerodynamics ripped it into pieces. One (I …
Saturn IB Launch: Looking for specific footage with engineer … 13 Sep 2024 · The segment ends with staging of SA-1, 2, or 3 AS-201 was a suborbital test of a heat shield with only a dummy upper stage. it can be distinguished from Apollo 1/7 by the …
Fireball at staging - NASASpaceFlight.com 27 Aug 2006 · Fireball at stagingMy guess is that most of the "fireball" at Saturn staging was due to the powerful upward-firing retrorockets on the first stage. You can see this effect in long …
Bringing back the Saturn V - NASASpaceFlight.com 27 Jul 2013 · The reason it had to be employed on the S-IVB of Saturn V is that staging occurred at a V a bit > 14,000 mph which meant that the 3rd stage still had to fight gravity losses.
Falcon Heavy 5 Vs. Saturn 5 - forum.nasaspaceflight.com 26 May 2011 · What would the possibility be for a Falcon Heavy with 5 cores or in other words a Falcon 5, with a central Falcon Heavy core and 4 Falcon Heavy outer cores not to be confused …
Stage Separation (Was: Hot-Staging) - NASASpaceFlight.com 22 Jun 2017 · For instance Saturn V had at least a dozen small solid-fuel motors for separation and ullage, each of which could have exploded and killed a mission. This is the only area …
Starship hot staging 6 Jul 2023 · It seems one of the primary issues driving the hot staging approach is ullage (particularly if that 10% payload increase is correct). Superheavy needs to keep its propellants …