Mission type | Climatology |
---|---|
Operator | NASA |
COSPAR ID | 2014-035A |
SATCAT no. | 40059 |
Website | JPL OCO-2 Mission |
Mission duration | 2 years (nominal) Elapsed: 9 years, 6 months, 29 days |
Spacecraft properties | |
Bus | LEOStar-2 |
Manufacturer | Orbital Sciences [1] |
Launch mass | 454 kg (1,001 lb) [1] |
Dry mass | 409 kg (902 lb) |
Payload mass | 131 kg (289 lb) [1] |
Dimensions | Stowed: 2.12 × 0.94 m (6.96 × 3.08 ft) [1] |
Power | 815 W [1] |
Start of mission | |
Launch date | 2 July 2014, 09:56:23 UTC |
Rocket | Delta II 7320-10C |
Launch site | Vandenberg, SLC-2W |
Contractor | United Launch Alliance |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Perigee altitude | 701.10 km (435.64 mi) |
Apogee altitude | 703.81 km (437.33 mi) |
Inclination | 98.2° |
Period | 98.82 minutes |
Mean motion | 14.57 rev / day |
Velocity | 7.5 km/s (4.7 mi/s) |
Epoch | 19 September 2016, 10:55:06 UTC [2] |
Revolution no. | 11,796 |
Main telescope | |
Type | Near-IR Cassegrain |
Focal ratio | ƒ/1.8 [3] |
Wavelengths | 2.06 microns 1.61 microns 0.765 microns [1] |
Instruments | |
3 grating spectrometers | |
Orbiting Carbon Observatory-2 (OCO-2) is an American environmental science satellite which launched on 2 July 2014. A NASA mission, it is a replacement for the Orbiting Carbon Observatory which was lost in a launch failure in 2009. It is the second successful high-precision (better than 0.3%) CO2 observing satellite, after GOSAT.
The OCO-2 satellite was built by Orbital Sciences Corporation, based around the LEOStar-2 bus. [4] The spacecraft is being used to study carbon dioxide concentrations and distributions in the atmosphere. [5]
OCO-2 was ordered after the original OCO spacecraft failed to achieve orbit. During the first satellite's launch atop a Taurus-XL in February 2009, the payload fairing failed to separate from around the spacecraft and the rocket did not have sufficient power to enter orbit with its additional mass. Although a Taurus launch was initially contracted for the reflight, the launch contract was cancelled after the same malfunction occurred on the launch of the Glory satellite two years later. [6]
United Launch Alliance launched OCO-2 using a Delta II rocket at the beginning of a 30-second launch window at 09:56 UTC (2:56 PDT) on 2 July 2014. Flying in the 7320-10C configuration, the rocket launched from Space Launch Complex 2W at Vandenberg Air Force Base. [7] The initial launch attempt on 1 July at 09:56:44 UTC was scrubbed at 46 seconds on the countdown clock due to a faulty valve on the water suppression system, used to flow water on the launch pad to dampen the acoustic energy during launch. [8]
OCO-2 joined the A-train satellite constellation, becoming the sixth satellite in the group. Members of the A-train fly very close together in Sun-synchronous orbit, to make nearly simultaneous measurements of Earth. A particularly short launch window of 30 seconds was necessary to achieve a proper position in the train. [9] As of 19 September 2016 it was in an orbit with a perigee of 701.10 km (435.64 mi), an apogee of 703.81 km (437.33 mi) and a 98.2° inclination. [2]
The mission is expected to cost US$467.7 million, including design, development, launch and operations. [1]
Rather than directly measuring concentrations of carbon dioxide in the atmosphere, OCO-2 records how much of the sunlight reflected off the Earth is absorbed by CO2 molecules in an air column. [10] OCO-2 makes measurements in three different spectral bands over four to eight different footprints of approximately 1.29 km × 2.25 km (0.80 mi × 1.40 mi) each. [11] [12] About 24 soundings are collected per second while in sunlight and over 10% of these are sufficiently cloud free for further analysis. One spectral band is used for column measurements of oxygen (A-band 0.765 microns), and two are used for column measurements of carbon dioxide (weak band 1.61 microns, strong band 2.06 microns). [3]
In the retrieval algorithm measurements from the three bands are combined to yield column-averaged dry-air mole fractions of carbon dioxide. Because these are dry-air mole fractions, these measurements do not change with water content or surface pressure. Because the molecular oxygen content of the atmosphere (i.e. excluding the oxygen in water vapour) is well known to be 20.95%, oxygen is used as a measure of the total dry air column. To ensure these measurements are traceable to the World Meteorological Organization, OCO-2 measurements are carefully compared with measurements by the Total Carbon Column Observing Network (TCCON). [3]
Mission data are provided to the public by the NASA Goddard Earth Science Data and Information Services Center (GES DISC). The Level 1B data product is the least processed and contains records for all collected soundings (about 74,000 soundings per orbit). The Level 2 product contains estimates of the column-averaged dry-air mole fractions of carbon dioxide, among other parameters such as surface albedo and aerosol content. The Level 3 product consists of global maps of carbon dioxide concentrations developed by OCO-2 scientists. [13]
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The Orbiting Carbon Observatory (OCO) is a NASA satellite mission intended to provide global space-based observations of atmospheric carbon dioxide. The original spacecraft was lost in a launch failure on 24 February 2009, when the payload fairing of the Taurus rocket which was carrying it failed to separate during ascent. The added mass of the fairing prevented the satellite from reaching orbit. It subsequently re-entered the atmosphere and crashed into the Indian Ocean near Antarctica. The replacement satellite, Orbiting Carbon Observatory-2, was launched 2 July 2014 aboard a Delta II rocket. The Orbiting Carbon Observatory-3, a stand-alone payload built from the spare OCO-2 flight instrument, was installed on the International Space Station's Kibō Exposed Facility in May 2019.
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Media related to Orbiting Carbon Observatory-2 at Wikimedia Commons