Meteor-M N2-1, D-Star ONE, SEAM
(No.980) Meteor-M N2-1, D-Star ONE, SEAM (2017年11月22日)
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(C)ROSCOSMOS
Launch: 2017.11.28, 05:41(UTC)
http://www.roscosmos.ru/24267/
http://www.wmo-sat.info/oscar/satellites/view/482
Composition of the associated load
Baumanets-2 spacecraft is manufactured by JSC VPK NPO
Mashinostroeniya on behalf of the federal state budget education
institution of higher professional education Moscow State Technical
University named after NE Bauman. "Baumanets-2" is designed for
remote sensing of the Earth's surface in the optical range,
providing experiments on the investigation of communication conditions
with the ground receiving station in the millimeter wave range.
amount 1 SC
Machine weight 86 kg
Life time 1 year
Height of working orbit 500-800 km
Mood 98 deg
LEO Vantage spacecraft was manufactured by the Canadian Space
Flight Laboratory of the Aerospace Research Institute of the University
of Toronto (UTIAS / SFL) commissioned by the Canadian company Telesat.
LEO Vantage is intended for testing and confirmation of further use
in a global, low-orbit satellite constellation with Ka-band.
amount 1 SC
Machine weight 70 kg
Life time 1 year
Height of working orbit 1000 km
Mood 98.48 deg
AISSat-3 spacecraft was manufactured by the Canadian company
Space Flight Laboratory (SpaceFlightLaboratory, Inc), commissioned
by the Norwegian Space Center (NorwegianSpaceCentre).
AISSat-3 is designed to receive signals from the Automatic
Recognition System (AIS) from ships.
amount 1 SC
Machine weight 6.5 kg
Life time 3 years
Height of working orbit 600-800 km
Mood 98 deg
IDEA spacecraft is designed for orbital observation of
submillimeter space debris. The manufacturer and end user of
IDEA is the Japanese company Astroskale (AstroscaleJapanInc).
amount 1 SC
Machine weight 22 kg
Life time 2 years 600-800 km
Height of working orbit
Mood 98.6 deg
SEAM spacecraft is designed to measure the Earth's magnetic
fields for scientific purposes (studying related processes in
the geospatial system). The manufacturer and end user of the
SEAM satellite is the Royal Institute of Technology (KTH)
represented by the Faculty of Cosmos and Plasma Physics (Sweden).
amount 1 SC
Machine weight 4.7 kg
Life time 1 year
Height of working orbit 600 km
Mood 98 deg
437.250MHz 9k6 GMSK
Landmapper-BC spacecraft is designed to collect multispectral
images for agricultural planning, water monitoring and land management.
The manufacturer and end user of each satellite type Landmapper-BC is
the American company AstroDigital (AstroDigital US Inc.).
amount 2 SC
Machine weight 11 kg
Life time 5 years
Height of working orbit 600 km
Mood 97.9 deg
LEMUR spacecraft is designed to monitor the movement of sea-going
vessels by receiving signals from the system of automatic vessel
recognition, weather forecasting based on radio-eclipsing measurements
of GPS signals (GPS-RO), aircraft monitoring by automatic dependent
surveillance (ADS-B) in peaceful purposes. The manufacturer and end
user of LEMUR satellites is the American company SpayerGlobal, Inc.
(SpireGlobal, Inc).
amount 10 SC
Machine weight 4.5 kg
Life time 2 years
Height of working orbit 600 km
Mood 98 deg
D-Star ONE spacecraft is designed for testing a new satellite
platform with a transceiver for the radio amateur service D-Star.
The manufacturer and end user of the satellite "D-Star ONE" is the
German company "German Orbital Systems GmbH" (GermanOrbitalSystemsGmbH).
amount 1 SC
Machine weight 3 kg
Life time 2 years
Height of working orbit 600 km
Mood 97.9 deg
Up 437.325MHz/Down 435.525MHz, Telemetry 435.700MHz
Planned flight program
UTC 28 Nov 2017
05:41:46 - Launch of the space rocket;
05:43:44 - Department of the 1st stage;
05:45:33 - Resetting the head fairing;
05:46:33 - Branch 2 steps;
05:51:09 - Head Unit Branch;
05:52:09 - 05:53:26 - RB "Frigate". Formation of the first transition orbit;
06:40:10 - 06:41:07 - the RB "Frigate". Formation of the orbit of the separation of spacecraft "Meteor-M";
06:42:08 - Department of spacecraft "Meteor-M" (orbit i = 98.57°, H = 828.7 km, h = 788.9 km);
07:21:01 - 07:21:24 - RB "Frigate". Formation of the second transition orbit;
08:01:43 - 08:05:03 - Department of spacecraft IDEA (orbit i = 97.95°, H = 814.2 km, h = 581.6 km);
08:13:21 - 08:13:37 - RB "Frigate". Formation of the orbit of the branch of the MCA group;
08:15:17 - Department of spacecraft "Baumanets" (orbit i = 97.76°, H = 600.1 km, h = 592.7 km);
08:20:00 - 08:35:00 - Separation of payload SEAM and spacecraft AISSat (orbit i = 97.76°, H = 601.8 km, h = 583.9 km);
08:59:21 - 08:59:44 - RB "Frigate". Formation of the third transition orbit;
09:50:01 - 09:50:46 - RB "Frigate". Formation of the orbit of the spacecraft LEO Vantage;
09:54:06 - Division of spacecraft LEO Vantage (orbit i = 99.46°, H = 1002.2 km, h = 996.8 km);
10:42:41 - 10:43:19 - Transfer of the accelerating unit to the trajectory of the entrance to the atmosphere;
~11:16:57 - The entry of the accelerating unit into the atmosphere (altitude 100 km). Flooding in the water area of the Pacific Ocean.
《補足》
打ち上げられましたが、分離に失敗しました。
(C)Roscosmos
Russia's Soyuz 2-1B rocket lifted off from the 1S launch pad at
the Vostochny Cosmodrome at 5:41 UTC on November 28, 2017 with the
Meteor-M 2-1 weather satellite and 18 small satellites riding as
secondary payloads. Becoming the second Soyuz to lift off from the
Eastern Spaceport, Soyuz 2-1B performed as planned but the mission
ran into trouble when handing over to the Fregat upper stage, failing to
achieve a stable orbit, reportedly as the result of a programming error.
http://www.d-star.one/
http://www.orbitalsystems.de/
http://twitter.com/GermanOrbital
http://www.facebook.com/germanorbitalsystems
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