任务档案 · MISSION

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蓝色起源 · 新格伦号 · 36A 号发射工位 (LC-36A)

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任务成功

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任务简介

New Glenn 运载火箭的首次飞行。将搭载原型 Blue Ring 有效载荷拖船和有效载荷吊装平台，该平台由通信阵列、电力系统和固定于次级有效载荷适配器环上的飞行计算机组成，并保持与第二级连接。此次发射将作为 New Glenn 的首次国家安全太空发射认证飞行。目标轨道为 2400 x 19300 公里，倾角 30°。

原文

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Maiden flight of the New Glenn launch vehicle. Will carry the prototype Blue Ring payload tug and payload hoisting platform, consisting of communications array, power systems, and a flight computer affixed to a secondary payload adapter ring, remaining attached to the 2nd stage. This launch will serve as New Glenn's first National Security Space Launch certification flight. Target orbit is 2400 x 19300 km at 30° inclination.

飞行时间线 Flight Timeline31 节点

T−04:30:00

二级 LH2 (液氢) 加注Stage 2 LH2 Load

Start of liquid hydrogen loading in the second stage

T−04:00:00

一级 LOX (液氧) 加注Stage 1 LOX Load

Start of liquid oxygen loading in the first stage

T−04:00:00

二级 LOX (液氧) 加注Stage 2 LOX Load

Start of liquid oxygen loading in the second stage

T−03:30:00

一级 LNG (液态甲烷) 加注Stage 1 LNG Load

Start of liquid methane loading in the first stage

T−01:00:00

发射直播开始Webcast live

Start of the launch broadcast

T−01:00:00

推进剂加注完成Prop Load Complete

End of propellant loading

T−20:00

天气状况检查Weather Check

Check of the weather conditions for launch

T−10:00

各岗位就绪查询Ready Poll

Polling ready ahead of terminal count

T−04:00

终端倒数开始Terminal Count

Start of the terminal countdown towards launch

T−02:30

燃料箱增压Tank Press

Fuel tanks are pressurized to flight levels

T−01:30

切换内部电源Internal Power

Launch vehicle switches to internal power sources

T−00:20

自动倒数启动Startup

The onboard computer takes control over the countdown and runs last checks

T−00:20

水帘降噪系统启动Water Deluge

Water deluge systems turn on

T−00:06

点火Ignition

Start of the engine ignition sequence

T+00:00

升空Liftoff

First upwards movement of the rocket

T+01:39

最大动压点Max-Q

Maximum dynamic pressure

T+03:10

主发动机关机MECO

Cut-off of the main engine

T+03:12

二级分离Stage 2 Separation

Separation of the second stage from the first

T+03:23

二级发动机第一次启动SES-1

First start of the second engine

T+03:46

卡门线 (100 km)Kármán Line

The vehicle crosses the Kármán Line (100 km altitude)

T+03:49

整流罩分离Fairing Separation

Separation of the payload fairing

T+07:17

再入减速点火Entry Burn Startup

Start of the atmospheric entry burn

T+07:45

再入减速关机Entry Burn Shutdown

End of the atmospheric entry burn

T+08:52

一级着陆减速点火Stage 1 Landing Burn

Start of the first stage landing burn

T+09:28

一级着陆Stage 1 Landing

Landing of the first stage

T+12:51

二级发动机第一次关机SECO-1

First cut-off of the second engine

T+13:51

载荷启动Payload Power On

Startup of the payload

T+57:42

二级发动机第二次启动SES-2

Second start of the second engine

T+58:58

二级发动机第二次关机SECO-2

Second cut-off of the second engine

T+01:59:18

二级姿态调整机动Stage 2 Orientation Maneuver

Stage 2 maneuver to change its attitude

T+05:50:58

任务结束Mission End

End of the launch vehicle's mission

任务更新38 条

16:5701/16

Cosmic_Penguin · 01/16

Launch success, 2nd stage and payload reached planned orbit.