BLITS: Difference between revisions
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'''BLITS (Ball Lens In The Space)''' is a [[Russia]]n satellite launched on September 17, 2009, as a secondary payload on a [[Soyuz-2 (rocket)|Soyuz-2.1b/Fregat]], from the Baikonur Cosmodrome in Kazakhstan. |
'''BLITS (Ball Lens In The Space)''' is a [[Russia]]n satellite launched on September 17, 2009, as a secondary payload on a [[Soyuz-2 (rocket)|Soyuz-2.1b/Fregat]], from the Baikonur Cosmodrome in Kazakhstan. |
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The satellite is totally passive and spherical, and is tracked using [[satellite laser ranging]] by the [[International Laser Ranging Service]]. The purpose of the mission is experimental verification of the spherical glass [[retroreflector]] satellite concept as well as |
The satellite is totally passive and spherical, and is tracked using [[satellite laser ranging]] (SLR) by the [[International Laser Ranging Service]]. The purpose of the mission is experimental verification of the spherical glass [[retroreflector]] satellite concept as well as SLR data for solution of scientific problems in geophysics, geodynamics, and relativity. The design of BLITS is based on the optical [[Luneburg lens]] concept. The retroreflector is a multilayer glass sphere; it provides uniform reflection characteristics when viewed within a very wide range of angles, and can provide a cross-section sufficient for observations at low to medium orbit heights. A similar design was already tested on a smaller laser reflector carried on board of the [[Meteor (satellite)|METEOR-3M]] spacecraft launched on December 10, 2001.<ref>{{cite web|title=Spherical Retroreflector with an Extremely Small Target Error: International Experiment in Space|url=http://cddis.nasa.gov/lw13/docs/papers/target_vasiliev_1m.pdf|work=13th International Workshop on Laser Ranging. Toward Millimeter Accuracy|publisher=[[NASA]]}}</ref> |
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The satellite body consists of two outer hemispheres (radius 85.16 mm) made of a low-refraction-index glass and an inner ball lens (radius 53.52 mm) made of a high-refraction-index glass; the two outer hemispheres and the inner ball are glued together, and one of the outer hemispheres is externally coated with a reflective coating, covered with a protective varnish. The total mass is 7.53 kg.<ref name="ILRS" /><ref name="EOportal">{{cite web|title=BLITS (Ball Lens In The Space)|url=https://directory.eoportal.org/web/eoportal/satellite-missions/b/blits|publisher=[[ESA]], Earth Observation portal}}</ref> |
The satellite body consists of two outer hemispheres (radius 85.16 mm) made of a low-refraction-index glass and an inner ball lens (radius 53.52 mm) made of a high-refraction-index glass; the two outer hemispheres and the inner ball are glued together, and one of the outer hemispheres is externally coated with a reflective coating, covered with a protective varnish. The total mass is 7.53 kg.<ref name="ILRS" /><ref name="EOportal">{{cite web|title=BLITS (Ball Lens In The Space)|url=https://directory.eoportal.org/web/eoportal/satellite-missions/b/blits|publisher=[[ESA]], Earth Observation portal}}</ref> |
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The satellite was inserted into an 832 km [[Sun-synchronous orbit]], with an inclination of 98.85º. The satellite was spinning at a spin period of 5.6 seconds around the axis normal to its orbit plane, allowing laser light to be reflected in short bursts because only half of the satellite is covered in a reflective coating. Being the satellite made of glass, minimum in-flight slowdown of spin rate was expected, as there were no conducting parts where currents interacting with the Earth magnetic field can be induced.<ref name="EOportal" /> |
The satellite was inserted into an 832 km [[Sun-synchronous orbit]], with an inclination of 98.85º. The satellite was spinning at a spin period of 5.6 seconds around the axis normal to its orbit plane, allowing laser light to be reflected in short bursts because only half of the satellite is covered in a reflective coating. Being the satellite made of glass, minimum in-flight slowdown of spin rate was expected, as there were no conducting parts where currents interacting with the Earth magnetic field can be induced.<ref name="EOportal" /> |
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Revision as of 04:14, 17 January 2019
 An artist's impression of BLITS | |
| Mission type | Technologie |
|---|---|
| Operator | Roskosmos ILRS |
| COSPAR ID | 2009-049G |
| SATCAT no. | 35871 |
| Mission duration | Achieved: 3 years Planned: 5 years |
| Spacecraft properties | |
| Manufacturer | FSUE-IPIE |
| Launch mass | 7.53 kilograms (16.6 lb) |
| Start of mission | |
| Launch date | 17 September 2009, 15:55:07 UTC[1] |
| Rocket | Soyuz-2-1b/Fregat |
| Launch site | Baikonur Site 31/6 |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Low Earth |
| Semi-major axis | 7,197.67 kilometres (4,472.42 mi) |
| Eccentricity | 0.0004373 |
| Perigee altitude | 823 kilometres (511 mi) |
| Apogee altitude | 829 kilometres (515 mi) |
| Inclination | 98.55 degrees |
| Period | 101.28 minutes |
| RAAN | 105.39 degrees |
| Epoch | 25 February 2014, 08:51:29 UTC[2] |
BLITS (Ball Lens In The Space) is a Russian satellite launched on September 17, 2009, as a secondary payload on a Soyuz-2.1b/Fregat, from the Baikonur Cosmodrome in Kazakhstan. The satellite is totally passive and spherical, and is tracked using satellite laser ranging (SLR) by the International Laser Ranging Service. The purpose of the mission is experimental verification of the spherical glass retroreflector satellite concept as well as SLR data for solution of scientific problems in geophysics, geodynamics, and relativity. The design of BLITS is based on the optical Luneburg lens concept. The retroreflector is a multilayer glass sphere; it provides uniform reflection characteristics when viewed within a very wide range of angles, and can provide a cross-section sufficient for observations at low to medium orbit heights. A similar design was already tested on a smaller laser reflector carried on board of the METEOR-3M spacecraft launched on December 10, 2001.[3] The satellite body consists of two outer hemispheres (radius 85.16 mm) made of a low-refraction-index glass and an inner ball lens (radius 53.52 mm) made of a high-refraction-index glass; the two outer hemispheres and the inner ball are glued together, and one of the outer hemispheres is externally coated with a reflective coating, covered with a protective varnish. The total mass is 7.53 kg.[1][4] The satellite was inserted into an 832 km Sun-synchronous orbit, with an inclination of 98.85º. The satellite was spinning at a spin period of 5.6 seconds around the axis normal to its orbit plane, allowing laser light to be reflected in short bursts because only half of the satellite is covered in a reflective coating. Being the satellite made of glass, minimum in-flight slowdown of spin rate was expected, as there were no conducting parts where currents interacting with the Earth magnetic field can be induced.[4] The expected operative life was at least 5 years, but the mission was interrupted in 2013 after a collision with space debris.[4][5]
Collision
On January 28, 2013, the International Laser Ranging Service announced that a collision happened between BLITS and a space debris fragment. As a result, an abrupt change occurred of the BLITS orbit parameters (a decrease of the orbiting period), and the spin period changed from 5.6 sec before collision to 2.1 sec after collision. On April 19, 2013 BLITS mission contacts from the Scientific Research Institute for Precision Instrument Engineering in Moscow asked the ILRS to end tracking on the satellite.[6] According to the simulation by the Center for Space Standards & Innovation (CSSI), a research arm of Analytical Graphics, Inc. (AGI), BLITS could have been hit by a piece of debris originated by the 2007 Chinese anti-satellite missile test.[7]
New version
An improved version of the reflector, named BLITS-M, is scheduled for launch in 2018 with the next Gonets-M mission.[8]
References
- ^ a b "BLITS". International Laser Ranging Service. Archived from the original on 2013-10-17. Retrieved 2014-02-25.
{{cite web}}: Unknown parameter|dead-url=ignored (|url-status=suggested) (help) - ^ "BLITS Satellite details 2009-049G NORAD 35871". N2YO. 25 February 2014. Retrieved 26 February 2014.
- ^ "Spherical Retroreflector with an Extremely Small Target Error: International Experiment in Space" (PDF). 13th International Workshop on Laser Ranging. Toward Millimeter Accuracy. NASA.
- ^ a b c "BLITS (Ball Lens In The Space)". ESA, Earth Observation portal.
- ^ "Russian BLITS Satellite hit by Space Debris". Spaceflight101.
- ^ "ILRS News". International Laser Ranging Service. (Scroll the page to read the news about 04/19/2013 of 02/28/2013).
- ^ Kelso, T.S. (March 8, 2013). "Chinese space debris may have hit Russian satellite". AGI Blog. AGI - Analytical Graphics, Inc. Archived from the original on March 11, 2013. Retrieved February 25, 2014.
{{cite web}}: Unknown parameter|dead-url=ignored (|url-status=suggested) (help) - ^ Krebs, Gunter. "BLITS-M". Gunter's Space Page. Retrieved 23 January 2017.
