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任务档案 · MISSION

GSAT-20 (GSAT-N2)

SpaceX · 猎鹰 9 Block 5 · 40 号发射工位 (SLC-40)

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任务简介

GSAT-20 是一颗印度地球静止轨道 Ka 波段高通量通信卫星。 GSAT 20 据称基于 I-6K 统一模块化总线建造,配备 Ka 波段高通量通信有效载荷,吞吐量达 70 Gbps,利用多个点波束为印度地区提供宽带服务。 它将是首颗完全采用电推进(EP)的卫星,效率可比化学推进高出五到六倍。它将是首颗使用电推进从地球静止转移轨道(GTO)进入地球同步轨道(GSO)的 ISRO 制造卫星。

原文
SpaceX

GSAT-20 is an Indian geostationary Ka-band high-throughput communications satellite. GSAT 20 is reportedly built on the I-6K unified modular bus and features a Ka-band high-throughput communications payload with 70 Gbps throughput utilizing multiple spot beams providing broadband services across the Indian region. It will be the first fully Electric Propulsion/EP enabled satellite which can be five to six times more efficient than chemical-based propulsion. It will be the first ISRO made satellite to move from Geostationary transfer orbit to Geosynchronous orbit using Electric Propulsion.

飞行时间线 Flight Timeline23 节点

T−38:00
加注决议通过GO for Prop Load
Launch director verifies go for propellant load
T−35:00
一级 LOX (液氧) 加注Stage 1 LOX Load
Start of liquid oxygen loading in the first stage
T−35:00
推进剂加注开始Prop Load
Start of propelland loading
T−16:00
二级 LOX (液氧) 加注Stage 2 LOX Load
Start of liquid oxygen loading in the second stage
T−07:00
发动机预冷Engine Chill
Start of engine chilling
T−01:00
燃料箱增压Tank Press
Fuel tanks are pressurized to flight levels
T−01:00
自动倒数启动Startup
The onboard computer takes control over the countdown and runs last checks
T−00:45
发射决议通过GO for Launch
Launch director verifies go for launch
T−00:03
点火Ignition
Start of the engine ignition sequence
T+00:00
升空Liftoff
First upwards movement of the rocket
T+01:11
最大动压点Max-Q
Maximum dynamic pressure
T+02:26
主发动机关机MECO
Cut-off of the main engine
T+02:30
二级分离Stage 2 Separation
Separation of the second stage from the first
T+02:36
二级发动机第一次启动SES-1
First start of the second engine
T+03:17
整流罩分离Fairing Separation
Separation of the payload fairing
T+06:13
再入减速点火Entry Burn Startup
Start of the atmospheric entry burn
T+06:39
再入减速关机Entry Burn Shutdown
End of the atmospheric entry burn
T+07:55
一级着陆减速点火Stage 1 Landing Burn
Start of the first stage landing burn
T+07:56
二级发动机第一次关机SECO-1
First cut-off of the second engine
T+08:20
一级着陆Stage 1 Landing
Landing of the first stage
T+26:41
二级发动机第二次启动SES-2
Second start of the second engine
T+27:47
二级发动机第二次关机SECO-2
Second cut-off of the second engine
T+33:58
载荷分离Payload Separation
Final deployment of the payload from the rocket

任务更新16

03:1911/19
Cosmic_Penguin · 11/18

Launch success with satellite in contact.

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03:0611/19
Cosmic_Penguin · 11/18

Spacecraft separation.

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02:3111/19
Cosmic_Penguin · 11/18

Liftoff.

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02:1211/19
LL2 · 11/18

Unofficial Webcast by SPACE AFFAIRS has started

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21:3911/17
Nosu · 11/17

Weather is >95% favorable for launch.

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06:1311/17
Nosu · 11/16

Setting GO

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06:5211/14
Cosmic_Penguin · 11/13

Updated launch window.

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22:1011/13
Cosmic_Penguin · 11/13

Tweaked launch window.

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07:5011/13
Cosmic_Penguin · 11/12

Moved up to November 18.

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13:5111/11
Cosmic_Penguin · 11/11

Targeting November 19.

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15:2011/09
Cosmic_Penguin · 11/09

Changed launch pad.

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10:4509/21
Cosmic_Penguin · 09/21

NET November.

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10:2209/04
Cosmic_Penguin · 09/04

NET end-of-2024.

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13:3006/19
Cosmic_Penguin · 06/19

NET August.

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11:2906/19
Cosmic_Penguin · 06/19

NET 2nd half of 2024.

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00:0601/03
hitura-nobad · 01/02

Payload moved to Falcon 9, targeting Q2 2024 for launch

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