HALCA (original) (raw)

From Wikipedia, the free encyclopedia

Japanese space radio telescope

For the Japanese singer, see Halca.

HALCA

HALCA after the final assembly during a solar battery check at Uchinoura
Names MUSES-BVSOPHaruka (はるか)
Mission type Astronomy
Operator ISAS
COSPAR ID 1997-005A Edit this at Wikidata
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)

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.

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. Spektr-R stopped operating in 2019.

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]

  1. ^ "HALCA (MUSES-B) Satellite details 1997-005A NORAD 24720". N2YO. 28 April 2016. Retrieved 28 April 2016.
  2. ^ ""Haruka" large antenna and space VLBI (「はるか」大型アンテナとスペースVLBI)". ISAS JAXA + translate.google.com. Retrieved 2020-01-24.
  3. ^ "VSOP newsletter number 161". Archived from the original on 2020-09-13. Retrieved 2012-02-17.
  4. ^ "Deployment of 8 m effective aperture antenna (有効口径8mアンテナの開発)". ISAS JAXA + translate.google.com. Retrieved 2020-01-24.
  5. ^ "Natori's Tears: Successful deployment of large antennas under tension (名取の涙──緊張の中、大型アンテナの展開成功)". ISAS JAXA + translate.google.com. Retrieved 2020-01-24.