REUSABLE LAUNCH VEHICLES

A reusable launch system (or reusable launch vehicle, RLV) is a launch system which is capable of launching a launch vehicle into space more than once. This contrasts with expendable launch systems, where each launch vehicle is launched once and then discarded.

No true orbital reusable launch system is currently in use. The closest example is the partially reusable Space Shuttle. The orbiter, which includes the main engines, and the two solid rocket boosters, are reused after several months of refitting work for each launch. The external fuel drop tank is typically discarded, but it is possible for it be re-used in space for various applications.

Orbital RLVs are thought to provide the possibility of low cost and highly reliable access to space. However, reusability implies weight penalties such as non-ablative reentry shielding and possibly a stronger structure to survive multiple uses, and given the lack of experience with these vehicles, the actual costs and reliability are yet to be seen.

It is a misconception that a number of technological breakthroughs are required before RLVs will be feasible. An American experimental RLV, the X-15, made its maiden flight on June 8, 1959. The X-15 was not called anRLV but ahypersonic airplane. It was incapable of reaching orbital speed (24,000 kilometers [15,000 miles] per hour) but flew fast enough (7,160 kilometers [4,475 miles] per hour) to reach an altitude above 100 kilometers (328,080 feet), the officially recognized boundary between Earth and space. In 199 flights the X-15 topped this altitude once, on August 22, 1963. With pilot Joe Walker at the controls, the X-15 reached 109,756 meters (360,000 feet) and became the first and only successful RLV.

The idea of the RLV can be traced back to 1928, and since that time a great many proposals have been made. The classic The Frontiers of Space (1969) vividly illustrates a number of RLV concepts, all of which were technically feasible at that time.