HALCA (Highly Advanced Laboratory for Communications and Astronomy), also known for its project name VSOP (VLBI Space Observatory Programme), the code name MUSES-B (for the second of the Mu Space Engineering Spacecraft series), or just Haruka (はるか)[2] was a Japanese 8 meter diameter radio telescope satellite which was used for Very Long Baseline Interferometry (VLBI). It was the first such space-borne dedicated VLBI mission.
![]() HALCA after the final assembly during a solar battery check at Uchinoura | |
Names | MUSES-B VSOP Haruka (はるか) |
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Mission type | Astronomy |
Operator | ISAS |
COSPAR ID | 1997-005A ![]() |
SATCAT no. | 24720 |
Website | HALCA Home |
Mission duration | 8 years, 9 months, 18 days |
Spacecraft properties | |
Manufacturer | NEC Toshiba Space Systems |
Launch mass | 830 kg (1,830 lb) |
Dimensions | 1.5 m × 1 m (4.9 ft × 3.3 ft) |
Start of mission | |
Launch date | 04:50, February 12, 1997 (UTC) (1997-02-12T04:50Z) |
Rocket | M-5-1 |
Launch site | Kagoshima M-V Pad |
End of mission | |
Disposal | decommissioned |
Deactivated | November 30, 2005 (2005-11-30) |
Orbital parameters | |
Reference system | Geocentric |
Regime | Highly elliptical |
Semi-major axis | 17,259 km (10,724 mi) |
Eccentricity | 0.5999671 |
Perigee altitude | 533.5 km (331.5 mi) |
Apogee altitude | 21,244.1 km (13,200.5 mi) |
Inclination | 31.1880 degrees |
Period | 376.1 minutes |
RAAN | 127.6566 degrees |
Argument of perigee | 143.9533 degrees |
Mean anomaly | 358.3371 degrees |
Mean motion | 3.82867831 rev/day |
Epoch | 28 April 2016, 09:56:58 UTC[1] |
Revolution no. | 26766 |
Main telescope | |
Type | Mesh antenna |
Diameter | 8 m (26 ft) |
Wavelengths | 1.3, 6, 18 cm (radio) |
It was placed in a highly elliptical orbit with an apogee altitude of 21,400 km and a perigee altitude of 560 km, with an orbital period of approximately 6.3 hours. This orbit allowed imaging of celestial radio sources by the satellite in conjunction with an array of ground-based radio telescopes, such that both good (u,v) plane coverage and very high resolution were obtained.
Although designed to observe in three frequency bands: 1.6 GHz, 5.0 GHz, and 22 GHz, it was found that the sensitivity of the 22 GHz band had severely degraded after orbital deployment, probably caused by vibrational deformation of the dish shape at launch, thus limiting observations to the 1.6 GHz and 5.0 GHz bands.
HALCA was launched in February 1997 from Kagoshima Space Center, and made its final VSOP observations in October 2003, far exceeding its 3-year predicted lifespan, before the loss of attitude control. All operations were officially ended in November 2005.[3]
A follow-up mission ASTRO-G (VSOP-2) was planned, with a proposed launch date of 2012, but the project was eventually cancelled in 2011 due to increasing costs and the difficulties of achieving its science goals. It was expected to achieve resolutions up to ten times higher and up to ten times greater sensitivity than its predecessor HALCA.
The cancellation of ASTRO-G left the Russian Spektr-R mission as the only then operational space VLBI facility.
The large 8 meter antenna was designed to unfold in space as the unfolded configuration did not fit inside the rocket fairing. The antenna was a metal mesh of 6000 cables. To form an ideal shape the length of the cables were adjusted on the backside of the antenna. One concern was that the cables could entangle.[4] The deployment of the main reflector started on February 27, 1997. The deployment was done over three hours on the first day and was completed in 20 minutes during the next day.[5]
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← 1996 · Orbital launches in 1997 · 1998 → | |
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STS-81 | GPS IIR-1 | GE 2 · Nahuel 1A | Soyuz TM-25 | STS-82 | Haruka | Kosmos 2337 · Kosmos 2338 · Kosmos 2339 · Gonets-D1 #4 · Gonets-D1 #5 · Gonets-D1 #6 | JCSAT-R | USA-130 | Intelsat 801 | Mozhayets 2 | Tempo-2 | STS-83 | USA-131 | Progress M-34 | Kosmos 2340 | Thaicom 3 · BSAT-1a | Kosmos 2341 | Minisat 01 · Founders | GOES 10 | Iridium 4 · Iridium 5 · Iridium 6 · Iridium 7 · Iridium 8 | Chinasat 6A | Kosmos 2342 | STS-84 | Kosmos 2343 | Tselina-2 | Thor 2 | Telstar 5 | Inmarsat-3 F4 · INSAT-2D | Kosmos 2344 | Feng Yun 2A | Iridium 9 · Iridium 10 · Iridium 11 · Iridium 12 · Iridium 13 · Iridium 14 · Iridium 16 | Intelsat 802 | STS-94 | Progress M-35 | Iridium 15 · Iridium 17 · Iridium 18 · Iridium 20 · Iridium 21 | USA-132 | Superbird-C | OrbView-2 | Soyuz TM-26 | STS-85 (CRISTA-SPAS) | PAS-6 | Kosmos 2345 | Agila 2 | Iridium 22 · Iridium 23 · Iridium 24 · Iridium 25 · Iridium 26 | Lewis | ACE | PAS-5 | FORTE | Iridium MFS-1 · Iridium MFS-2 | Hot Bird 3 · Meteosat 7 | GE-3 | Iridium 27 · Iridium 28 · Iridium 29 · Iridium 30 · Iridium 31 · Iridium 32 · Iridium 33 | Kosmos 2346 · FAISAT-2V | Intelsat 803 | Molniya-1T #98 | STS-86 | Iridium 19 · Iridium 34 · Iridium 35 · Iridium 36 · Iridium 37 | IRS-1D | Progress M-36 (Sputnik 40 · X-Mir) | EchoStar III | Foton #11 | Cassini (Huygens) | Apstar 2R | USA-133 | STEP-4 | USA-135 · FalconGOLD | Maqsat-B · Maqsat-H · YES | SCD-2A | USA-134 | USA-136 | Iridium 38 · Iridium 39 · Iridium 40 · Iridium 41 · Iridium 43 | Kupon | Sirius 2 · IndoStar-1 | Resurs-F1M #1 | STS-87 (SPARTAN-201) | TRMM · Orihime · Hikoboshi | JCSAT-1B · Equator-S | Astra 1G | Iridium 42 · Iridium 44 | Galaxy 8i | Kosmos 2347 | Kosmos 2348 | Progress M-37 | Iridium 45 · Iridium 46 · Iridium 47 · Iridium 48 · Iridium 49 | Intelsat 804 | Orbcomm FM5 · Orbcomm FM6 · Orbcomm FM7 · Orbcomm FM8 · Orbcomm FM9 · Orbcomm FM10 · Orbcomm FM11 · Orbcomm FM12 | Early Bird 1 | AsiaSat 3 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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