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Information such as the date and time, launch pad, and payload for a rocket launch are presented through this infobox. It is designed with a heading, image syntax, fourteen cell parameters divided into two distinct sections, and succession. The syntax used in this template is fairly simple, and uses four {{#if:}} parser functions.
Rocket and payload of last landing --> | rockets = <!-- rockets that have used the pad -->}}}} Legacy (obsolete) parameters These parameters are supported by the template to allow it to display properly on articles that have not yet been converted to the new format.
A model rocket is a small rocket designed to reach low altitudes (e.g., 100–500 m (330–1,640 ft) for a 30 g (1.1 oz) model) and be recovered by a variety of means. According to the United States National Association of Rocketry (NAR) 's Safety Code, [ 1 ] model rockets are constructed out of lightweight and non metallic parts.
The Falcon 9 v1.0 first stage was used on the first five Falcon 9 launches, and powered by nine SpaceX Merlin 1C rocket engines arranged in a 3x3 pattern. Each of these engines had a sea-level thrust of 556 kN (125,000 pounds-force) for a total thrust on liftoff of about 5,000 kN (1,100,000 pounds-force).
A launch pad is an above-ground facility from which a rocket-powered missile or space vehicle is vertically launched. [1] The term launch pad can be used to describe just the central launch platform ( mobile launcher platform ), or the entire complex ( launch complex ).
A flame trench can also be used in combination with a diverter to form a trench-deflector system. The flames from the rocket travel through openings in the launchpad onto a flame deflector situated in the flame trench, which runs underneath the launch structure and extends well beyond the launchpad itself. [3]
The Mobile Launcher Platform-1 on top of a crawler-transporter. A mobile launcher platform (MLP), also known as mobile launch platform, is a structure used to support a large multistage space vehicle which is assembled (stacked) vertically in an integration facility (e.g. the Vehicle Assembly Building) and then transported by a crawler-transporter (CT) to a launch pad.
The Installation and Testing Building (Монтажно-испытательный корпус, Montazhno-ispytatel'nyj korpus) named "Site No.2" was built and a special railway completed from there to Site No.1 where the launch pad for the rocket was located. [5] By April 1957, all remaining work was completed and the site was ready for launches.