Brovane
Diamond Member
- Dec 18, 2001
- 6,370
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what ever happened with the group that was redesigning the Saturn V's F1 engines using modern tooling? thought they were getting ridiculous thrust out of them.
http://arstechnica.com/science/2013/04/how-nasa-brought-the-monstrous-f-1-moon-rocket-back-to-life/
I would make a trip to see a heavy lift platform akin to the Saturn V with those F-1's tearing up the sky, people say the sound/concussion from shuttle launches were a joke compared to them.
They are still in play for the Advanced Booster program for SLS.
NASA will eventually switch from Shuttle-derived five-segment SRBs to upgraded boosters[29] These may be of either the solid rocket or liquid rocket booster type.[13] NASA originally planned to incorporate these advanced boosters in the Block IA configuration of SLS, but this was superseded by Block IB, which will continue to use five-segment SRBs combined with a new upper stage,[30] after it was determined that the Block IA configuration would result in high acceleration which would be unsuitable for Orion and could result in a costly redesign of the Block I core.[31] Prior to the selection of Block IB, NASA intended to begin the Advanced Booster Competition,[3][32][33] which would have selected an advanced booster in 2015. Though NASA is no longer planning on selecting new boosters for the first flights of SLS,[34] competitors for the advanced booster include:
Aerojet, in partnership with Teledyne Brown, with a domestic version of an uprated Soviet NK-33 LOX/RP-1 engine, an engine derived from the NK-15 initially designed to lift the unsuccessful N-1 Soviet moonshot vehicle, with each engine's thrust increased from 394,000 lbf (1.75 MN) to at least 500,000 lbf (2.2 MN) at sea level. This booster would be powered by eight AJ-26-500 engines,[35] or four AJ-1E6 engines[36] On February 14, 2013, NASA awarded a $23.3 million 30-month contract Aerojet to build a full-scale 550,000-pound thrust class main injector and thrust chamber to be used in the advanced booster.[37] Two standard Aerojet AJ-26 engines, together producing a combined 735,000 lbf (3.27 MN) of sea level thrust, successfully lifted the Antares rocket in 2013.[38]
Pratt & Whitney Rocketdyne and Dynetics, with a booster design known as "Pyrios", which would use two F-1B engines derived from the F-1 LOX/RP-1 engine that powered the first stage of the Saturn V vehicle in the Apollo program. In 2012, it was determined that if the dual-engined Pyrios booster was selected for the SLS Block II, the payload could be 150 metric tons (t) to Low Earth Orbit, 20 t more than the baseline 130 t to LEO for SLS Block II.[39] In 2013, it was reported that in comparison to the F-1 engine that it is derived from, the F-1B engine is to have improved efficiency, be more cost effective and have fewer engine parts.[40] Each F-1B is to produce 1,800,000 lbf (8.0 MN) of thrust at sea level, an increase over the 1,550,000 lbf (6.9 MN) of thrust of the initial F-1 engine.[41]
ATK proposed an advanced SRB named "Dark Knight" with more energetic propellant, a lighter composite case, and other design improvements to reduce costs and improve performance. ATK states it provides "capability for the SLS to achieve 130 t payload with significant margin" when combined with a Block II core stage containing five RS-25 engines. However, the advanced SRB would achieve no more than 113 t to low earth orbit with the current core stage with four RS-25 engines.[3][39][42]
Christopher Crumbly, manager of NASAs SLS advanced development office in January 2013 commented on the booster competition, "The F-1 has great advantages because it is a gas generator and has a very simple cycle. The oxygen-rich staged combustion cycle [Aerojets engine] has great advantages because it has a higher specific impulse. The Russians have been flying ox[ygen]-rich for a long time. Either one can work. The solids [of ATK] can work."[43]