Search results
Results From The WOW.Com Content Network
The article is organized into two tables: the first contains a list of currently active and under-development launcher families, while the second contains a list of retired launcher families. The related article " Comparison of orbital launch systems " lists each individual launcher system within any given launcher family, categorized by its ...
[note 2] Liquid-propellant rockets have a motor that feeds liquid propellant(s) into a combustion chamber. Most liquid engines use a bipropellant , consisting of two liquid propellants (fuel and oxidizer) which are stored and handled separately before being mixed and burned inside the combustion chamber.
The topic of this article may not meet Wikipedia's notability guideline for stand-alone lists. Please help to demonstrate the notability of the topic by citing reliable secondary sources that are independent of the topic and provide significant coverage of it beyond a mere trivial mention.
Danish PULS-lauchner with EXTRA type missile pods. It can be configured to carry a variety of rockets in two sealed pod containers: 36 (2 pods × 18 rockets each) 122mm Grad rockets; or 26 (2×13) 160mm LAR-160 or ACCULAR rockets; or eight (2×4) 306mm EXTRA rockets; two (2×1) 330mm Delilah missiles or four (2×2) 370mm Predator Hawk tactical ballistic missiles.
A two-stage-to-orbit (TSTO) or two-stage rocket is a launch vehicle in which two distinct stages provide propulsion consecutively in order to achieve orbital velocity. It is intermediate between a three-stage-to-orbit launcher and a hypothetical single-stage-to-orbit (SSTO) launcher.
The Shavit launcher is developed by Malam factory, one of four factories in the IAI Electronics Group. The factory is very experienced in development, assembling, testing and operating system for use in space. The Shavit is a triple-stage launcher solid propellant booster based on the 2-stage Jericho-II ballistic missile.
A RIM-156A missile launching from a VLS cell on USS Lake Erie in 2008. US Navy Mark 41 Tomahawk hot launch. 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.
The rocket had a diameter of 1.6 m (5 ft 3 in) for the first stage and 1.3 m (4 ft 3 in) for the second stage and payload fairing. [ 4 ] On the 24th of October 2019, the company announced plans to develop a three-stage variant that would be capable of launching 100 kg (220 lb) to the Moon , 70 kg (150 lb) to Venus , or 50 kg (110 lb) to Mars .