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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
Pakistan's sounding rocket program used a variety of sounding rockets which were renamed in 3 series. Some flights were not given a Pakistani designation. Sounding rockets were flown from the Sonmiani Rocket Range.
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.
Aerojet Rocketdyne proposed in 2014 to "lobby the government to fund an all-new, U.S.-sourced rocket propulsion system." In June 2014, Aerojet initially projected it would cost under US$25 million per pair of engines, not including the up to US$1 billion estimated development cost to be funded by the government.
RS-56 (Rocket System-56) was an American liquid-fueled rocket engine, developed by Rocketdyne. RS-56 was derived from the RS-27 rocket engine, [1] which itself is derived from the Rocketdyne H-1 rocket engine used in the Saturn I and Saturn IB. Two variants of this engine were built, both for use on the Atlas II rocket series.
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 first stage of the H–I was a licence-built version of the Thor-ELT, which was originally constructed for the US Delta 1000 rocket. The stage had already been produced under licence in Japan for the N-I and N-II rockets. The second stage was entirely Japanese, using an LE-5 engine, the first rocket engine in Japan to use a cryogenic fuel.