Hiten (spacecraft)

Hiten-Hagoromo

Hiten spacecraft
Names	MUSES-A (before launch)
Operator	ISAS
COSPAR ID	1990-007A
SATCAT no.	20448
Website	ISAS Hiten page
Mission duration	3 years, 2 months and 17 days
Spacecraft properties
Launch mass	197 kg[1]
Start of mission
Launch date	11:46, January 24, 1990 (UTC) (1990-01-24T11:46Z)
Rocket	Mu-3S-II (no. 5)
Launch site	Uchinoura Space Center
End of mission
Decay date	18:03:25.7, April 10, 1993 (UTC) (1993-04-10T18:03:25.7Z)
Flyby of Moon
Closest approach	20:04:09, March 18, 1990
Distance	16,472.4 km (10,235.5 mi)
Moon orbiter
Orbital insertion	13:33, February 15, 1993
Orbital parameters
Periselene altitude	6.52 Lunar radii
Aposelene altitude	29.42 Lunar radii
Inclination	34.7°
Moon impactor
Impact date	18:03:25.7, April 10, 1993
Impact site	34°18′S 55°36′E / 34.3°S 55.6°E / -34.3; 55.6

The Hiten spacecraft (ひてん, Japanese pronunciation: [çiteɴ]), given the English name Celestial Maiden^[2] and known before launch as MUSES-A (Mu Space Engineering Spacecraft A), part of the MUSES Program, was built by the Institute of Space and Astronautical Science of Japan and launched on January 24, 1990.^[3] It was Japan's first lunar probe, the first robotic lunar probe since the Soviet Union's Luna 24 in 1976, and the first lunar probe launched by a country other than the Soviet Union or the United States.^[4][5] The spacecraft was named after flying heavenly beings in Buddhism.^[6]

Hiten was to be placed into a highly elliptical Earth orbit with an apogee of 476,000 km, which would swing past the Moon. However, the injection took place with a delta-v deficit of 50 m/s, resulting in an apogee of only 290,000 km.^[3] The deficiency was corrected and the probe continued on its mission.

On the first lunar swing-by, Hiten released a small orbiter, Hagoromo (はごろも, named after the feather mantle of Hiten), into lunar orbit. The transmitter on Hagoromo failed, and even though ignition of Hagoromo's deceleration rockets was confirmed by ground observation, it could never be confirmed if the spacecraft had successfully inserted itself into lunar orbit or failed to capture, entering a heliocentric orbit.^[7] After the eighth swing-by, Hiten successfully demonstrated the aerobraking technique on March 19, 1991, flying by the Earth at an altitude of 125.5 km over the Pacific at 11.0 km/s. Atmospheric drag lowered the velocity by 1.712 m/s and the apogee altitude by 8665 km.^[8] This was the first aerobraking maneuver by a deep space probe.^[9]: 2 After the ninth lunar swing-by and second aerobraking maneuver on March 30, 1991, the primary mission of the probe was concluded.