 IBEX satellite | |
| Names | Explorer 91 IBEX SMEX-10 |
|---|---|
| Mission type | Astronomy |
| Operator | NASA |
| COSPAR ID | 2008-051A |
| SATCAT no. | 33401 |
| Website | ibex |
| Mission duration | 2 years (planned) 16 years, 22 days (in progress) |
| Spacecraft properties | |
| Spacecraft | Explorer XCI |
| Spacecraft type | Interstellar Boundary Explorer |
| Bus | MicroStar-1 |
| Manufacturer | Orbital Sciences Corporation |
| Launch mass | 107 kg (236 lb) [1] |
| Dry mass | 80 kg (180 lb) |
| Payload mass | 26 kg (57 lb) |
| Dimensions | 58 × 95 cm (23 × 37 in) |
| Power | 116 watts |
| Start of mission | |
| Launch date | 19 October 2008, 17:47:23 UTC |
| Rocket | Pegasus XL (F40) |
| Launch site | Bucholz Airfield, Stargazer |
| Contractor | Orbital Sciences Corporation |
| Entered service | January 2009 |
| Orbital parameters | |
| Reference system | Geocentric orbit[2] |
| Regime | High Earth orbit |
| Perigee altitude | 7,000 km (4,300 mi) |
| Apogee altitude | 220,886 km (137,252 mi) |
| Inclination | 10.99° |
| Period | 6604.00 minutes |
| Instruments | |
| IBEX-Lo IBEX-Hi | |
 IBEX mission logo Explorer program | |
Interstellar Boundary Explorer (IBEX or Explorer 91 or SMEX-10) is a NASA satellite in Earth orbit that uses energetic neutral atoms (ENAs) to image the interaction region between the Solar System and interstellar space. The mission is part of NASA's Small Explorer program and was launched with a Pegasus-XL launch vehicle on 19 October 2008.[3]
The mission is led by Dr. David J. McComas (IBEX principal investigator), formerly of the Southwest Research Institute (SwRI) and now with Princeton University. The Los Alamos National Laboratory and the Lockheed Martin Advanced Technology Center built the IBEX-Hi and IBEX-Lo sensors respectively. The Orbital Sciences Corporation manufactured the satellite bus and was the location for spacecraft environmental testing. The nominal mission baseline duration was two years after commissioning, and the prime ended in early 2011. The spacecraft and sensors are still healthy and the mission is continuing in its extended mission.[4]
IBEX is in a Sun-oriented spin-stabilized orbit around the Earth.[5] In June 2011, IBEX was shifted to a new, more efficient, much more stable orbit.[6] It does not come as close to the Moon in the new orbit, and expends less fuel to maintain its position.[6]
The spacecraft is equipped with two large aperture imagers which detect ENAs with energies from 10 eV to 2 keV (IBEX-Lo) and 300 eV to 6 keV (IBEX-Hi).
The mission was originally planned to be a 24-month operations period. The mission has since been extended, with the spacecraft still in operation as of 2024[update].
- ^ "IBEX". ESA. Retrieved 13 August 2015.
- ^ "Trajectory: IBEX (Explorer 91) 2008-051A". NASA. 28 October 2021. Retrieved 9 December 2021.
This article incorporates text from this source, which is in the public domain.
- ^ Ray, Justin (19 October 2008). "Mission Status Center: Pegasus/IBEX". Spaceflight Now. Retrieved 27 November 2009.
- ^ "Archived Updates". Southwest Research Institute.
- ^ "Fact Sheet: IBEX" (PDF). Orbital ATK. FS001_06_3695. Archived from the original (PDF) on 16 March 2015. Retrieved 27 April 2015.
- ^ a b Cite error: The named reference
ibexnews201111was invoked but never defined (see the help page).
