Please make a donation to support Gunter's Space Page.
Thank you very much for visiting Gunter's Space Page. I hope that this site is useful and informative for you.
If you appreciate the information provided on this site, please consider supporting my work by making a simple and secure donation via PayPal. Please help to run the website and keep everything free of charge. Thank you very much.

Etalon 1, 2

Etalon 1

Etalon are a Soviet / Russian family (Etalon-1, Etalon-2) of passive geodetic satellites dedicated to satellite laser ranging. Etalon-1 was the first geodynamic satellite launched by the former Soviet Union. The Etalon spacecraft were launched in 1989 in conjunction with a pair of GLObal'naya NAvigatisionnay Sputnikovaya Sistema (GLONASS) satellites. The mission objectives were to determine a high accuracy terrestrial reference frame and earth rotation parameters; to improve the gravity field, and to improve the gravitational constant.

The Etalon satellites are passive satellites. The only instrumentation is the retro-reflector array which consists of 2 different type of cube corners.

RetroReflector Array (RRA) Characteristics:
Each Etalon satellite is a 1.294 m diameter sphere. The diameter of the sphere touching the corner cube reflector (CCR) faces is 1284 mm (the difference does not cause any masking). There are a total of 2140 fused-quartz CCR's (304 arrays 7 CCR's each and 2 arrays 6 CCR's each) plus 6 germanium CCR's. Each CCR has the same dimensions and is made of the same material (fused quartz). The same CCRs were used on GLONASS.

The satellite surface is made of aluminum-titanium alloy with an integral coefficient of diffuse reflectivity 0.7 (on average), but IPIE before-launch measurements show some difference when observed from different directions, so there can be some brightness variation during the satellite rotation. The CCR distribution over the satellite surface is not absolutely uniform for technological reasons (some space is needed for the holders and separation device), so the correction value relative to the CoM (which is within +3 mm from the sphere center) may vary for different observation directions. For the same reason, there is also a small variation in the equivalent optical cross-sections (no more than +15 %, according to the measurement results). The mean correction value is 562.0 mm with an RMS error for various observation directions 11.35 mm. All the CCR's have aluminum-coated reflecting surface.

Nation: USSR
Type / Application: Geodesy
Operator:
Contractors:
Equipment: RetroReflector array
Configuration: 1.294 m sphere
Propulsion: None
Power: None
Lifetime:
Mass: 1415 kg
Orbit: 19095 km × 19156 km, 65.24 (#1); 19097 km × 19146 km, 65.35 (#2)
Satellite COSPAR Date LS Launch Vehicle Remarks
Kosmos 1989 (Etalon #1) 1989-001C 10.01.1989 Ba LC-200/39 Proton-K Blok-DM-2 with Kosmos 1987 (Uragan #32), Kosmos 1988 (Uragan #33)
Kosmos 2024 (Etalon #2) 1989-039C 31.05.1989 Ba LC-200/40 Proton-K Blok-DM-2 with Kosmos 2022 (Uragan #34), Kosmos 2023 (Uragan #35)