QUESTION: Does the launcher's second stage have a restartable capability? How are the cut-off and restart are controlled? ANSWER from Andrew Petro on December 9, 1997: Not all launch vehicle second stages have engines with re-start capability. First of all, many launch vehicles have more than two stages and for those there would not be any need to re-start the 2nd stage. But it is a good question because most launch vehicles follow a path in which the rocket shuts down and coasts partway around the Earth and then the rocket has to fire again to place the spacecraft into a circular orbit. This can either be done by having a separate final stage (it could be the 2nd, 3rd, 4th, etc.) that does this burn or the final stage must be re-started to do this burn. The Space Shuttle uses its small orbital maneuvering engines to do this. Once the rocket is coasting in space, it is in free-fall (weightless) so the liquid oxidizer and fuel will just float around inside their tanks. To re-start the engines, the fuel and oxidizer in the tanks must either be behind a pressurized bladder so that it is forced to flow to the engine or there must be a way to move the propellants to the end of the tank that feeds the engine. Sometimes small engines (with their own pressurized propellant supply) are fired to create an artificial gravity force to move the propellants to the big engine so that it can be started. Many satellites have final stages with solid propellant which is not affected by the weightlessness. With some kinds of propellant, actually re-starting the engines in space is done the same way as on Earth, using something like a spark plug to ignite the oxidizer and fuel. Many rockets have final stages which use a special kind of propellant which is hypergolic, which means that the oxidizer and fuel are so reactive with each other that they ignite on contact and don't require any spark. Naturally you have to be careful handling this stuff. The Space Shuttle uses hypergolic propellants for its small orbital maneuvering and control rockets. There are valves in the lines which carry the oxidizer and fuel to the engine and these valves are opened when you want the engine to fire and they are closed to make the engine shut down. Andrew Petro Johnson Space Center