The tsiolkovsky rocket equation, classical rocket equation, or ideal rocket equation, describes the motion of vehicles that follow the basic principle of a rocket: a device that can apply acceleration to itself using thrust by expelling part of its mass with high velocity and thereby move due to the conservation of momentum.. The standard missile-3 (sm-3) is an exo-atmospheric missile defense interceptor used for theater ballistic missile defense. which allows for a higher burnout velocity, allowing the interceptor to travel farther and intercept missiles travelling at faster speeds. this expands the range of the system and the number of targets it can engage.. The velocity attained by a missile at the point of burnout. want to thank tfd for its existence? tell a friend about us, add a link to this page, or visit the webmaster's page for free fun content.
![LGM-118A [MX] Peacekeeper ICBM United States Nuclear Forces](https://www.globalsecurity.org/wmd/systems/images/lgm-118-line1.gif "Orbital’s Minotaur V launches LADEE mission to the Moon ...")
Ballistic missile basics a ballistic missile (bm) is a a missile that has a ballistic trajectory over most of its flight path, regardless of whether or not it is a weapon-delivery vehicle.. For example, a 6000-km range missile would need a 6200 m/sec burnout velocity and could achieve this while devoting 2-5% of its gross weight to payload; a 10,000-km range missile would need 7200 m/sec and could devote 1.3-3.5% of its weight to payload, about two-thirds as much.. Rocket motor design and missile flight performance analysis - download as pdf file (.pdf), text file (.txt) or view presentation slides online. some guidelines on rocket motor design.
