Note:
(a)
(i) The report is locked behind paywall.
(ii) The take-home lesson is that US is not good at everything.
(iii) There is no need to read the rest, which is not available for free anyway.
(b) RD-180 (RD is the two-letter acronym of two words in Russian for "Rocket Engine"/ table: Manufacturer NPO Energomash + thrust at vacuum and sea level are 4.15 MN and 3.83 MN, respectively, where MN = meganewton; mega = million) / "It features a dual combustion chamber, dual-nozzle design and is fueled by a kerosene/LOX mixture" (LOX = liquid oxygen) Wikipedia
(i) Wikipedia says its production is "1999-2014." It is plain wrong with regard to 2014. The engine remains in production, which is just the common sense. Otherwise where can Pentagon get new supply?
(ii) RD-180 first in use was in 2000.
(iii) meaning of manufacturer name:
Brian Harvey, Russia in Space; The failed frontier? Springer, 2001, at page 253
https://books.google.com/books?i ... rgomash&f=false
("NPO Energomash, its current name, or to be more precise, Energomash imemi Valentin Glushko (Energomash, dedicated to the memory of Valentin Glushko)" )
Russian full name and its English translation.
(iv)
(A) "Thrust is a reaction force described quantitatively by Isaac Newton's second and third laws. * * * Force, and thus thrust, is measured in the International System of Units (SI) as the newton (symbol: N), and represents the amount needed to accelerate 1 kilogram of mass at the rate of 1 meter per second per second." Wikipedia for "thrust"
(B) "Since they need no external material to form their jet, rocket engines can perform in a vacuum and thus can be used to propel spacecraft and ballistic missiles." Wikipedia for "rocket engine"
(c) "The first payload launched with an Atlas V was the Hot Bird 6 communications satellite launched from Cape Canaveral * * * into geostationary transfer orbit (GTO) on August 21, 2002." Wikipedia for "Atlas V"
(d)
(i) Falcon Heavy. SpaceX, undated
http://www.spacex.com/falcon-heavy
(ii) Merlin Engines. SpaceX, undated
www.spacex.com/news/2013/03/26/merlin-engines
("The Merlin engine that powers the first stage of Falcon 9 is developed and manufactured in-house by SpaceX. Burning liquid oxygen and rocket-grade kerosene propellant, a single Merlin engine emits 845 kilonewtons (190,000 pounds) of thrust at liftoff, rising to 914 kilonewtons (205,500 pounds) as it climbs out of Earth's atmosphere. Merlin's thrust-to-weight ratio exceeds 150, making the Merlin the most efficient booster engine ever built")
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