Nozomi (spacecraft)

Nozomi
Artist's concept of Nozomi orbiter at Mars
NamesPLANET-B
Mission typeMars orbiter
OperatorJAXA
COSPAR ID1998-041A Edit this at Wikidata
SATCAT no.25383
Websiteisas.jaxa.jp
Mission duration5 years, 5 months and 6 days
Spacecraft properties
ManufacturerISAS
Launch mass540 kg (1,190 lb)[1]
Dry mass225 kg (496 lb)
Payload mass33 kg (73 lb)[1]
Dimensions1.6 × 1.6 × 0.58 m (5.2 × 5.2 × 1.9 ft)[1]
Start of mission
Launch dateJuly 3, 1998, 18:12:00 UTC
RocketM-V
Launch siteUchinoura Space Center
End of mission
DisposalDecommissioned
DeactivatedDecember 31, 2003
Last contactDecember 9, 2003
Orbital parameters
Reference systemHeliocentric
Transponders
FrequencyX-band: 8410.93 MHz
S-band: 2293.89 MHz
PLANET series
← Suisei

Nozomi (Japanese: のぞみ, lit. "Wish" or "Hope", and known before launch as Planet-B) was a Japanese Mars orbiter that failed to reach Mars due to electrical failure. It was constructed by the Institute of Space and Astronautical Science, University of Tokyo and launched on July 4, 1998, at 03:12 JST (July 3, 1998, at 18:12 UTC) with an on-orbit dry mass of 258 kg and 282 kg of propellant.[citation needed] The Nozomi mission was terminated on December 31, 2003.[citation needed]

Nozomi was designed to study the upper Martian atmosphere and its interaction with the solar wind and to develop technologies for use in future planetary missions. Specifically, instruments on the spacecraft were to measure the structure, composition and dynamics of the ionosphere, aeronomy effects of the solar wind, the escape of atmospheric constituents, the intrinsic magnetic field, the penetration of the solar-wind magnetic field, the structure of the magnetosphere, and dust in the upper atmosphere and in orbit around Mars. The mission would have also returned images of Mars' surface.[citation needed]

  1. ^ a b c "Nozomi". NASA Space Science Data Coordinated Archive. Retrieved December 1, 2022.