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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 [ 4 ] [ 5 ] [ 3 ] [ 6 ] [ 1 ] [ 7 ]
Titus (rocket) This page was last edited on 14 November 2023, at 13:03 (UTC). Text is available under the Creative Commons Attribution-ShareAlike 4.0 License ...
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).
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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 XM47 (large fins) was only an interim rocket, essentially a rocket test vehicle, and was used for training and testing purposes only. DoD video showing MGR-3 Little John in army-testing in 1957, including transport by CH-37 helicopter. Carried on the XM34 rocket launcher, it could carry either nuclear or conventional warheads.
The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.