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Estes Industries was founded by Vernon Estes in 1958; in 1961, the company moved to a 77-acre tract of land on the outskirts of Penrose, Colorado. [10] [1] In 1969, Vernon sold the company to the Damon Corporation of Needham, Massachusetts, a company which also purchased a number of other hobby companies including a smaller competitor of Estes, Centuri Engineering of Phoenix, Arizona.
Engine Origin Designer Vehicle Status Use Propellant Power cycle Specific impulse (s) [a] Thrust (N) [a] Chamber pressure (bar) Mass (kg) Thrust: weight ratio [b] Oxidiser: fuel ratio
The Saturn V reached 400 feet per second (120 m/s) at over 1 mile (1,600 m) in altitude. Much of the early portion of the flight was spent gaining altitude, with the required velocity coming later. The Saturn V broke the sound barrier at just over 1 minute at an altitude of between 3.45 and 4.6 miles (5.55 and 7.40 km). At this point, shock ...
Saturn C-5N: NASA: 1972 Saturn INT-20: UR-700: Vladimir Chelomei: Saenger (spacecraft) Eugen Sänger, Junkers, MBB, DLR: 1995 Saturn C-8: NASA: 1962 1962 Sea Dragon: Robert Truax: Douglas SASSTO: Philip Bono: 1967 Martin Marietta Spacemaster: Martin Marietta: Saturn V-A: NASA: 1968 Saturn V-C: Saturn V-Centaur: Saturn V-D: Saturn INT-21: 1970s ...
This Saturn IB second-stage Auxiliary Propulsion Unit is similar to one used on the Saturn V third stage, which performed as an ullage engine for translunar injection. Ullage motors (also known as ullage engines or ullage rockets ) are relatively small, independently fueled rocket engines that may be fired prior to main engine ignition, when ...
During their two and a half minutes of operation, the five F-1s propelled the Saturn V vehicle to a height of 42 miles (222,000 ft; 68 km) and a speed of 6,164 mph (9,920 km/h). The combined flow rate of the five F-1s in the Saturn V was 3,357 US gal (12,710 L) [ 5 ] or 28,415 lb (12,890 kg) per second.
The American Saturn MLV family of rockets was proposed in 1965 by NASA as successors to the Saturn V rocket. [71] It would have been able to carry up to 160,880 kg (354,680 lb) to low Earth orbit. The Nova designs were also studied by NASA before the agency chose the Saturn V in the early 1960s [ 72 ] Nova was cancelled in 1964 and had reusable ...
Ares V Lite was a scaled down Ares V. [27] [28] It would have used five RS-68 engines and two five-segment SRBs and have had a low Earth orbit payload of approximately 140 tonnes (310,000 lb). [29] If chosen, Ares V Lite would have replaced the Ares V and Ares I launchers. One Ares V Lite version would have been a cargo lifter like Ares V and ...
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