Thank you for that. Now, please indicate what impact the kerosene shown above is having upon the steel and the concrete onto which it is depositing its fury?
The exhaust plume for the Saturn V stack impinged upon a steel flame deflector weighing approximately 600 tons
1,2 and coated with a replaceable ceramic ablator
3, which diverted the exhaust into two 58-foot wide flame
2 trenches lined with reinforced concrete and firebrick. A water deluge
1 system dumped approximately 10,000 gallons of water onto the deflector over about a half-minute period. The Launch Umbilical Tower base and deck received an additional approximately 30,000 gallons of water over the same period. The deluge system provided not only cooling but also suppression of acoustic energy which could otherwise have inflicted significant damage to the vehicle and ground equipment. An additional 20,000 gallons per minute was supplied to the LUT base and deck for several more minutes after launch, and an additional several thousand gallons per minute were used to fog the tower for cooling through nozzles at several levels.
Now, of course, the RP-1/LO
2 propellant mixture energy went largely into providing 7.5 million lbf thrust and thus pushing a few thousand tons rapidly into the sky (you know, the rocket thingy). But, even despite the heavy construction of the facilities, purpose-built to endure the launch conditions, the cooling and acoustic-suppression systems, and the transitory nature of the launch, there was certainly
some damage. The facility required refurbishing after each launch. I don't know how much, exactly; coming up with a specific description would require additional research. If you're interested, I'll provide you with an hourly rate...
Or, let me put it thi way, sts, would you agree with me that the awesome display of kerosene that you posted is not doing any damage whatsoever to the concrete, much less the steel it is coming into contact with?
No, of course not; but the point is irrelevant anyway. Are you comparing the effect of approximately fifteen seconds' worth of rocket launch on facilities described above to the effect of high-speed airliner impact, and subsequent jet fuel and contents fires, on a
skyscraper? Really? If you'd like to do so, feel free to start another thread.
On
this thread, we're still waiting for you to specify your claim, or to offer any
specific objections to the studies refuting your premise, or to address the numerous other errors and self-contradictions in your claims.
Sources:
1. NASA TMX-65237, Apollo/Saturn V Facility Description, Vol. II: Launch Complex 39 Facility Description, NASA/KSC: 1 October 1966.
2. Apollo press kits (e.g., Apollo 13 press kit, available at http://science.ksc.nasa.gov/history/apollo/apollo-13/docs/apollo-13-press-kit.txt)
3. Saturn V News Reference (Facilities), NASA: December 1968 update.