# 发射台[编辑]

位於美國佛罗里达梅里特岛的LC-39B号发射台

**发射台**是一种设计为发射火箭能驱动飞行器的地面设施（包括运载火箭、航天飞机、弹道导弹等在内），可用于固定和支撐火箭並为火箭和载荷提供维护支持。發射台大致可分為固定式發射台和移動式發射台，其中移動式發射台可以在公路或铁路上进行移動。

大多数发射台都包括固定的服务结构，以提供一个或多个进入平台来组装、检查和维护运载工具，并允许进入航天器，包括装载机组人员。 该垫可以包含火焰偏转结构，以防止火箭排气的强热损坏飞行器或垫结构，并且可以采用喷洒大量水的声音抑制系统。 该垫也可以受到避雷器的保护。 航天发射场通常包括多个发射场和其他支持基础设施。

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已隱藏部分未翻譯内容，歡迎參與翻譯。
Most launch pads include fixed service structures to provide one or more access platforms to assemble, inspect, and maintain the vehicle and to allow access to the spacecraft, including the loading of crew. The pad may contain a flame deflection structure to prevent the intense heat of the rocket exhaust from damaging the vehicle or pad structures, and a sound suppression system spraying large quantities of water may be employed. The pad may also be protected by lightning arresters. A spaceport typically includes multiple launch complexes and other supporting infrastructure.

The launch complex for liquid fueled rockets often has extensive ground support equipment including propellant tanks and plumbing to fill the rocket before launch. Cryogenic propellants (liquid oxygen oxidizer, and liquid hydrogen or liquid methane fuel) need to be continuously topped off (i.e., boil-off replaced) during the launch sequence (countdown), as the vehicle awaits liftoff. This becomes particularly important as complex sequences may be interrupted by planned or unplanned holds to fix problems.

Most rockets need to be supported and held down for a few seconds after ignition while the engines build up to full thrust. The vehicle is commonly held on the pad by hold-down arms or explosive bolts, which are triggered when the vehicle is stable and ready to fly, at which point all umbilical connections with the pad are released.

## Transport of rockets to the pad

Transport of Soyuz rocket to pad by train
Transport of Space Shuttle and MLP to pad on Crawler-transporter
SLC-40 with SpaceX Falcon 9 launch infrastructure. The four towers surrounding the rocket are lightning arresters, and acts like a giant Faraday cage.
Each launch site is unique, but a few broad types can be described by the means by which the space vehicle gets to the pad.

* Horizontally integrated rockets travel horizontally with the tail forward to the launch site on a transporter erector launcher and are then raised to the vertical position over the flame duct. Examples include all large Soviet rockets, including Soyuz, Proton, N1, and Energia. This method is also used by the SpaceX and Electron launch vehicles.
* Silo launched rockets are assembled inside of a missile silo. This method is only used by converted ICBMs due to the difficulty and expense of constructing a silo that can contain the forces of a rocket launch.
* Vertically integrated rockets can be assembled in a separate hangar on a mobile launcher platform (MLP). The MLP contains the umbilical structure and is carried to the launch site on a large vehicle called Crawler-transporter. Launch Complex 39 at the Kennedy Space Center is an example of a facility using this method. A similar system is used to launch Ariane 5 rockets at ELA-3 at Guiana Space Centre.
* Vertically assembled vehicles can also be transported on a mobile launcher platform resting on two parallel standard gauge railroad tracks that run from the integration building to launch area. This system is still in use for the Atlas V and future Vulcan.
* At SLC-6 and SLC-37, rockets are assembled on the launch mount. A windowless rail-mounted building encloses the launch pad and gantry to protect the vehicle from the elements, and for purposes of military secrecy. Prior to launch, the building is rolled away. This method is also used at Kagoshima for the M-V.
* The former Sea Launch service used the converted self-propelled oil drilling platform *Ocean Odyssey* to transport Zenit 3SL rockets horizontally to the Equator, and then to erect and launch them from a floating launch platform into geostationary transfer orbits.

## 选址

发射台的建设始于选址，需要考虑火箭的目标轨道（决定了发射方向）和残骸落区范围，以及各种地理和后勤因素。就目标轨道而言，通常情况下，将发射台建在低纬度地区，最好位于赤道，有利于充分利用地球自转速度来提高发射速度至入轨速度。但对于极地轨道和莫尔尼亚轨道等高倾角轨道，则正好相反，此时应该尽量选择纬度较高的地点。同样，如果是发射较为罕见的逆行轨道卫星，由于需要克服地球自转的线速度，高纬度地点理论上更加合适。就残骸落区而言，火箭上升阶段不能经过人口稠密地区，最好是飞行在海洋上方，以避免正常或异常残骸造成的危险。考虑到这两点，发射台往往位于东临海洋的海岸，如肯尼迪航天中心、种子岛宇宙中心和文昌航天发射场。

理论上，高空发射的优势在于垂直飞行距离更短，火箭更容易穿过稀薄的大气层。然而，发射场的海拔高度并非航天发射场选址的主要决定因素，因为发射所需的大部分速度增量（Δv）都用于达到所需的水平轨道速度。几公里额外高度带来的微小增益通常不足以抵消在山区进行地面运输的后勤成本。

## 发射台的类型

其中综合发射系统通常包括一个用于支撑火箭的发射架或发射平台（即狭义上的“发射台”）、一个带有脐带缆的服务结构（通称“脐带塔”），以及一套用于提供推进剂、电力、通信、遥测、散热、火箭组装、有效载荷处理和存储设施所需的勤务设施（通称“勤务塔”），而以上所述的各个结构在实际设计时其功能可能会被合并至同一个建筑中去（如921发射工位的发射塔架便集成了勤务塔和脐带塔的功能）。

* 运载火箭
* 发射场
* 發射場列表
* 导弹发射井
* 地面设施
* 發射塔架
* 发射台中止试验
* 运输起竖发射车
* 非火箭航天发射