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HAYABUSA 2 (40319)
COSPAR: 2014-076A | Alt Name: Hayabusa 2
DECAYED
Image
Additional Sources
Launch Details
Launch Date
December 3, 2014
Launch Site
TANSC
Launch Pad
Y
Launch Vehicle
H-IIA 202
Orbital Elements
NORAD ID
40319
International Designator
2014-076A
Decay Date
Unknown
Basic Satellite Info
Name
HAYABUSA 2
Alternative Name
Hayabusa 2
Type
Payload
Status
Extended mission
Owner
ISASJ
Country
Japan
Constellation
N/A
Related Satellites
Major Events
N/A
Summary
HAYABUSA 2 (OBJECT_ID: 2014-076A) is an asteroid lander and sample return satellite launched on December 3, 2014, from Tanegashima Space Center in Japan using the H-IIA 202 launch vehicle. The spacecraft has dimensions of 1.6 meters in length, 1 meter in diameter, and spans up to 6 meters with its solar arrays deployed. It had a dry mass of 446 kilograms and launched with a total mass of 554 kilograms. Manufactured by ISASJ (Institute of Space and Astronautical Science Japan Aerospace Exploration Agency), HAYABUSA 2 is equipped with a sampler and reentry capsule for its mission objectives. The satellite's power system consists of two deployable fixed solar arrays and batteries. It was designed to operate for approximately six years, aiming to collect samples from the asteroid Ryugu and return them to Earth.
Physical Characteristics
Length
1.6
Diameter
1
Span
6
Dry Mass
446
Launch Mass
554
Shape
Box+2 pan+boom
Radar Cross Section
4.4212
Visual Magnitude
Unknown
Color
Unknown
Material Composition
Unknown
Technical Details
Payload
Hayabusa-2
Purpose
Asteroid lander and sample return
Mission
Asteroid lander and sample return
Manufacturer
ISASJ
Life Expectancy
6 years
Bus
MUSES
Configuration
Unknown
Motor
AOCS
Equipment
Sampler, reentry capsule
Power System
2 deployable fixed solar arrays, batteries
ADCS
Unknown
Transmitter Frequency
Unknown
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