Extreme Ultraviolet Explorer
Extreme Ultraviolet Explorer (EUVE)
The EUVE spacecraft |
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Mission type |
Astronomical observation |
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Operator |
NASA |
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COSPAR ID |
1992-031A |
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SATCAT № |
21987 |
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Mission duration |
9 years |
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Spacecraft properties |
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Bus |
Multimission Modular Spacecraft |
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Dry mass |
3,275 kilograms (7,220 lb) |
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Start of mission |
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Launch date |
June 7, 1992, 16:40:00 (1992-06-07UTC16:40Z) UTC |
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Rocket |
Delta 6920-X[1] |
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Launch site |
Cape Canaveral LC-17A[1] |
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End of mission |
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Deactivated |
31 January 2001 (2001-02-01) |
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Decay date |
30 January 2002 |
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Orbital parameters |
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Reference system |
Geocentric |
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Regime |
Low Earth |
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Eccentricity |
0.01152 |
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Perigee |
515 kilometers (320 mi) |
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Apogee |
527 kilometers (327 mi) |
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Inclination |
28.4 degrees |
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Period |
94.8 minutes |
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Epoch |
11 July 1992[2] |
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The Extreme Ultraviolet Explorer (EUVE) was a space telescope for ultraviolet astronomy, launched on June 7, 1992. With instruments for ultraviolet (UV) radiation between wavelengths of 7 and 76 nm, the EUVE was the first satellite mission especially for the short-wave ultraviolet range. The satellite compiled an all-sky survey of 801 astronomical targets before being decommissioned on January 31, 2001. It re-entered the atmosphere on January 30, 2002.[3]
Mission goals
The goals of the mission included several different areas of observation using the extreme ultraviolet (EUV) range of frequencies:
- To make an all-sky survey in the extreme ultraviolet band
- To make a deep survey in the EUV range on two separate bandpasses
- To make spectroscopic observations of targets found by other missions
- To observe EUV sources such as hot white dwarfs and coronal stars
- To study the composition of the interstellar medium using EUV spectroscopy
- To determine whether it would be beneficial to create another, more sensitive EUV telescope
![](../I/m/EUVE.jpg)
The Extreme Ultraviolet Explorer Spacecraft prior to launch
Payload instruments
NASA describe these:[4]
- 2 Wolter-Schwarzschild Type I grazing incidence mirror, each with an imaging microchannel plate (MCP detector)(Scanner A & B) FOV ~5° diameter; two passbands 44-220 Å 140-360 Å
- 1 Wolter-Schwarzschild Type II grazing incidence mirror, with an imaging microchannel plate (MCP detector) FOV ~4° diameter; two passbands 520-750 Å 400-600 Å
- 1 Wolter-Schwarzschild Type II grazing incidence mirror Deep Survey/Spectrometer Telescope. The light is split, with half of the light fed to:
- An imaging Deep Survey MCP detector [and the other half to ]
- Three Spectrometers which are each combinations of a grating and MCP detector: SW (70-190 Å) MW (140-380 Å) LW (280-760 Å).
See also
References
External links
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| Current | |
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| Planned | |
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| Proposals | |
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| Completed | |
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| Lost | |
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| Completed |
- hibernating after mission: SWAS (1998–2005)
- TRACE (1998–2010)
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| On hiatus | |
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| Cancelled | |
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| See also | |
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Category
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- Italics indicates probes that failed to deploy or otherwise malfunctioned
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| Kosmos 2175 | STS-42 | Kosmos 2176 | Progress M-11 | Kosmos 2177 · Kosmos 2178 · Kosmos 2179 | Unnamed | USA-78 | Fuyo 1 | Kosmos 2180 | USA-79 | Superbird B1 · Arabsat 1C | Molniya 1-83 | Kosmos 2181 | Galaxy 5 | Soyuz TM-14 | STS-45 | Kosmos 2182 | Gorizont No.36L | Kosmos 2183 | USA-80 | Kosmos 2184 | Telecom 2B · Inmarsat-2 F4 | Progress M-12 | USA-81 | Resurs-F2 No.8 | Kosmos 2185 | STS-49 | Palapa B4 | SROSS-C | Kosmos 2186 | Kosmos 2187 · Kosmos 2188 · Kosmos 2189 · Kosmos 2190 · Kosmos 2191 · Kosmos 2192 · Kosmos 2193 · Kosmos 2194 | EUVE | Intelsat K | Resurs-F1 No.55 | STS-50 | Progress M-13 | Kosmos 2195 | USA-82 | SAMPEX | USA-83 | Kosmos 2196 | INSAT-2A · Eutelsat-2 F4 | Kosmos 2197 · Kosmos 2198 · Kosmos 2199 · Kosmos 2200 · Kosmos 2201 · Kosmos 2202 | Gorizont No.37L | Geotail · DUVE | Kosmos 2203 | Soyuz TM-15 | Kosmos 2204 · Kosmos 2205 · Kosmos 2206 | Kosmos 2207 | STS-46 ( EURECA · TSS-1) | Molniya 1-84 | FSW-13 | TOPEX/Poseidon · Uribyol 1 · S80/T | Kosmos 2208 | Optus B1 | Progress M-14 | Resurs-F1 No.54 · Pion-Germes 1 · Pion-Germes 2 | Galaxy 1R | Satcom C4 | USA-84 | Kosmos 2209 | Hispasat 1A · Satcom C3 | STS-47 | Kosmos 2210 | Mars Observer | FSW-14 · Freja | Foton No.8L | DFS-Kopernikus 3 | Molniya-3 No.50 | Kosmos 2211 · Kosmos 2212 · Kosmos 2213 · Kosmos 2214 · Kosmos 2215 · Kosmos 2216 | Kosmos 2217 | STS-52 (LAGEOS-2 · CTA) | Progress M-15 (Znamya-2) | Galaxy 7 | Kosmos 2218 | Ekran-M No.15L | Resurs 500 | Kosmos 2219 | Kosmos 2220 | MSTI-1 | USA-85 | Kosmos 2221 | Kosmos 2222 | Gorizont No.38L | USA-86 | Superbird A1 | Molniya-3 No.56 | STS-53 (USA-89 · ODERACS) | Kosmos 2223 | Kosmos 2224 | USA-87 | Optus B2 | Kosmos 2226 | Kosmos 2225 | Kosmos 2227 | Kosmos 2228 | Kosmos 2229 | | Payloads are separated by bullets ( · ), launches by pipes ( | ). Manned flights are indicated in bold text. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in brackets. |
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