JCSAT-2B
, known as
JCSAT-14
before commissioning, is a
geostationary
communications satellite
operated by
SKY Perfect JSAT Group
and designed and manufactured by
SSL
on the
SSL 1300
platform.
[4]
[5]
It had a launch weight of 4,696.2 kg (10,353 lb), a power production capacity of 9 to 9.9 kW at end of life and a 15-year design life.
[3]
Its payload is composed of 26
C band
and 18
K
u
band
transponders
with a total bandwidth of 2,853 MHz.
[3]
SKY Perfect JSAT Group will use JCSAT-2B as a replacement for
JCSAT-2A
to provide communications services to Japan, Asia, Russia, Oceania, and the Pacific Islands.
[5]
History
[
edit
]
On June 11, 2013,
SSL
announced that it had been awarded a contract by
SKY Perfect JSAT Group
to manufacture
JCSAT-14
. It would be a 10 kW satellite with 26
C band
and 18
K
u
band
transponders with a 15 years of expected life. It was scheduled for launch in 2015.
[6]
On January 10, 2014, JSAT announced that it had signed a launch service contract with
SpaceX
for the launch of JCSAT-14 aboard a
Falcon 9
rocket. The expected launch date was the second half of 2015.
[7]
But the failure of
Falcon 9 Flight 19
meant a delay of at least six months on the launch.
[3]
On March 14, 2016, SSL delivered JCSAT-14 to the launch site, at
Cape Canaveral Air Force Station
, for launch processing and integration.
[8]
JCSAT-14 was launched on May 6, 2016, at 05:21 UTC by a
Falcon 9
rocket.
[3]
The next day, SSL announced that the satellite had deployed the solar arrays, was in full control and was performing orbital maneuvers to reach its operational position.
[9]
Since July 2016, the rechristened JCSAT-2B is commissioned and operational at the
154° East
orbital slot.
[10]
Launch and rocket landing
[
edit
]
JCSAT-14 was launched to
geostationary transfer orbit
on May 6, 2016, at 05:21 UTC, as the 24th mission of a
Falcon 9 Full Thrust
rocket.
[3]
The rocket's first stage subsequently landed on the
autonomous spaceport drone ship
Of Course I Still Love You
in the Atlantic Ocean.
[11]
The first stage of the rocket encountered "extreme temperatures during its reentry into Earth atmosphere" and was subsequently identified as a candidate for reflight, and as a "reference vehicle" for further testing. It was subjected to a series of tests, including a 150-second full-duration engine firing completed on 28 July 2016. Additional tests were planned before SpaceX determines the stage's suitability for reuse on a subsequent launch.
[12]
SpaceX has since completed at least 7 more full-duration firings of the core, and has indicated that this stage will be used solely for ground testing purposes.
[
citation needed
]
See also
[
edit
]
References
[
edit
]
External links
[
edit
]
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Launch designations
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Operational designations
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January
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February
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March
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April
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May
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June
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July
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August
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September
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October
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November
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December
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- Progress MS-04
- Gokturk-1
- Resourcesat-2A
- WGS-8
- HTV-6
/
Kounotori 6
, (
EGG, TuPOD, UBAKUSAT, AOBA-VELOX, STARS, FREEDOM, ITF, Waseda-SAT, OSNSAT,
Tancredo-1
, TechEDSat,
Lemur-2
× 4
)
- Fengyun 4A
- CYGNSS
× 8
- EchoStar 19
- Arase
/ ERG
- TanSat
,
Spark
× 2
- Star One D1
,
JCSAT-15
- SuperView
/ Gaojing-1 01, 02,
Bayi Kepu
1
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Launches are separated by dots ( ? ), payloads by commas ( , ), multiple names for the same satellite by slashes ( / ).
Crewed flights
are underlined. Launch failures are marked with the † sign. Payloads deployed from other spacecraft are (enclosed in parentheses).
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