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This comparison of orbital launch systems lists the attributes of all current and future individual rocket configurations designed to reach orbit. A first list contains rockets that are operational or have attempted an orbital flight attempt as of 2024; a second list includes all upcoming rockets.
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
Nulka is an Australian-designed and -developed active missile decoy built by an American/Australian collaboration. [1] [2] Used aboard warships of the United States Navy, Royal Australian Navy, United States Coast Guard and Royal Canadian Navy, [3] Nulka is a rocket-propelled, disposable, offboard, active decoy designed to lure anti-ship missiles away from their targets.
Sea Launch was founded by four companies from four countries, which shared the original ownership of offshore Cayman Islands-registered Sea Launch.Ship "Sea Launch" registered Monrovia [22] after reorganising from Chapter 11 bankruptcy in 2010, a majority share of the company was acquired by Russian interests.
Design and development of the missile began in 1983 when Goodyear Aerospace was contracted by the U.S. Navy to develop a ship-launched anti-submarine missile compatible with the new Mark 41 vertical launching system (VLS). The development of the VLS ASROC underwent many delays, and it was not deployed on any ships until 1993.
The earliest space vehicles were expendable launch systems, using a single or multistage rocket to carry a relatively small spacecraft in proportion to the total vehicle size and mass. [1] An early exception to this, the Space Shuttle , consisted of a reusable orbital vehicle carrying crew and payload, supported by an expendable external ...
The Scaled Composites Model 316, [2] known as SpaceShipOne, was a spaceplane designed to: . Carry three humans (one of them a pilot) in a sea-level pressurized cabin.; Be propelled by rocket from an altitude of 15 km (9.3 mi) to in excess of 100 km (62 mi).
The first sortie carried the rocket and launcher, and the second sortie fired an inert, unguided rocket to ensure the weapon would separate from the aircraft. Two armed rockets were fired during the third sortie from 10,000 and 15,000 feet. The second rocket launched into a 70 knot headwind, and both impacted within inches of the target.