Cold Launch vs. Hot Launch


Last Updated on 01/29/2020 by OTC

Launching a missile isn’t as easy as pressing the red button. It takes a lot of engineering and science to ensure safe firing.  In this article we will try to explain firing methods from Vertical Launch Systems (VLS).  VLS use two different methods for firing.

A vertical launch system can be either hot launch, where the missile ignites in the cell, or cold launch, where the missile is expelled by gas produced by a gas generator which is not part of the missile itself, and then the missile ignites. “Cold” means relatively cold compared with rocket engine exhaust. A hot launch system does not require an ejection mechanism, but does require some way of disposing of the missile’s exhaust and heat as it leaves the cell. If the missile ignites in a cell without an ejection mechanism, the cell must withstand the tremendous heat generated without igniting the missiles in the adjacent cells.

An advantage of a hot-launch system is that the missile propels itself out of the launching cell using its own engine, which eliminates the need for a separate system to eject the missile from the launching tube. This potentially makes a hot-launch system relatively light, small, and economical to develop and produce, particularly when designed around smaller missiles. A potential disadvantage is that a malfunctioning missile could destroy the launch tube.

Hot Launch

The advantage of the cold-launch system is in its safety: should a missile engine malfunction during launch, the cold-launch system can eject the missile thereby reducing or eliminating the threat. For this reason, Russian VLSs are often designed with a slant so that a malfunctioning missile will land in the water instead of on the ship’s deck. As missile size grows, the benefits of ejection launching increase. Above a certain size, a missile booster cannot be safely ignited within the confines of a ship’s hull. Most modern ICBMs and SLBMs are cold-launched.

Cold Launch

Hot launch systems have much faster engagement times as the missile is released from the ship almost immediately after the motor is ignited, whereas with a cold launch system, the missile must first be ejected from the launch cell and then ignited, thus extending the launch time. Further, cold launch systems do not require a hot exhaust gas management system but do require a gas, piston, or elevator ejection system, which could introduce additional mechanical reliability concerns.

The primary hazard with hot launch systems is the risk of a restrained firing. Likewise, cold launch systems have the risk of ejecting the missile without subsequent rocket motor ignition, potentially resulting in the ejected missile falling back onto the deck of the ship.

There are also hybrid VLS systems enables cold launch from hot launch systems, like ExLS. Lockheed Martin Extensible Launching System (ExLS) enables cold launch of Common Anti-Air Modular Missile (CAMM), or Sea Ceptor, from the Mk 41 VLS.

Lockheed Martin Extensible Launching System (ExLS)

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