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Titus was derived from the initial two stages of the Bérénice test vehicle. [2] [4]The first stage, weighing 1935 kg, used a SEPR-739-2 Stromboli solid rocket motor with 1245 kg of Plastolane propellant with a 20-second burn time.
Las Palmas (also mentioned as Lapachito and Chaco) [1] is a rocket launch site in Argentina at used on November 12, 1966, [2] for the launch of two Titus rockets [3] for observing a solar eclipse
The Rocketdyne S-3D (Air Force designation LR79) [1] [2] is an American liquid rocket engine produced by Rocketdyne (a division of North American Aviation) between 1956 and 1961. It was a gas generator, pump-fed engine, using a liquid oxygen ( LOX ) and RP-1 (kerosene) propellant combination, capable of producing 134908 pounds of thrust (600.1 ...
Bérénice was 13.25 m (43.5 ft) long, possessed a diameter of 0.56 m (1.8 ft) and weighed 3,340 kg (7,360 lb) at launch. The takeoff thrust of Bérénice, which could carry a payload of 3,340 kg (7,360 lb) to a height of 1,000 km (620 mi), amounted to 170 kN (38,000 lbf).
ALCO RS-3, diesel locomotive built by American Locomotive Company and Montreal Locomotive Works; Aprilia RS Cube, also known as the RS 3, a 2002–2004 Italian MotoGP race bike; RS3 my bruthaaa top level vehicle for light weight drag racing. The 5 cylinder provided from this little machine is very durable and tunable for tuning.
The containerized launch system and rocket can be deployed to and launched from a suitably flat site, the main requirements being access for trucks capable of carrying up to 16 m (52 ft)-long ISO containers (for the RS-1 first stage), and a flat concrete pad 46 m (151 ft) x 15 m (49 ft).
One of the main goals of SLI was to develop components of a reusable launch vehicle with high reliability. The RS-83 was designed for a loss of vehicle rate of 1 in 1,000. Another goal of the program was to dramatically reduce the cost per unit weight of payload to low Earth orbit. The RS-83 was designed with the goal of $1,000/lb ($2,200/kg).
The RS-27 (Rocket System-27) was a liquid-propellant rocket engine developed in 1974 by Rocketdyne to replace the aging MB-3 in the Delta. Incorporating components of the venerable MB-3 and the H-1 designs, the RS-27 was a modernized version of the basic design used for two decades.