The spacecraft payload consists of the following instruments:
The C/NOFS Occultation Receiver for Ionospheric Sensing and Specification (CORISS) is a Global Positioning System (GPS) dual-frequency receiver that measures the total electron content (TEC) along the line-of-sight from C/NOFS to GPS satellite. TEC measurement can help to constrain C/NOFS ionospheric models. Limb profiles of TEC obtained during occultations can be inverted to produce vertical profiles of electron density. It may be also possible to measure L-band scintillations caused by electron density irregularities.2
The Coherent Electromagnetic Radio Tomography (CERTO) is a tri-band (150, 400, 1067 MHz) radio beacon that permits direct measurement of ionospheric scintillation parameters at several frequencies by ground receivers. CERTO measurements can also be used for tomographic reconstruction of electron density profiles.3
The Coupled Ion-Neutral Dynamics Investigation (CINDI) payload is funded by NASA as an Explorer Mission of Opportunity. CINDI consists of two instruments: the Ion Velocity Meter (IVM) and the Neutral Wind Meter (NWM). The IVM instrument includes an ion drift meter and a retarding potential analyzer. IVM measure the ion drift vector, the ion temperature, and the major ion composition with a spatial resolution of about 4 km (2.5 mi) along the satellite track; the ion drift meter also provides vertical and horizontal ion drift components at 500 m (1,600 ft) resolution. The NWM consists of a cross track wind sensor and a ram wind sensor providing a direct measure of the neutral wind vector with a spatial resolution of about 8 km (5.0 mi) along the satellite track.4
The Planar Langmuir Probe (PLP) is a dual-disk probe designed to provide in situ measurements of plasma density and density fluctuations. Low time-resolution density measurements are intended as inputs for background ionosphere models and high time-resolution density irregularity measurements to specify disturbance conditions. PLP also monitors the spacecraft surface potential.5
The Vector Electric Field Instrument (VEFI) consists primarily of three orthogonal 20 m (66 ft) tip-to-tip double probe antennas. It measures the alternating current (AC) and Direct current (DC) electric fields related to plasma drift and irregularity development. The VEFI instrument package also includes a fluxgate magnetometer, an optical lightning detector and a fixed-bias Langmuir probe.6
C/NOFS science data is available online for general use. VEFI and PLP data are available through NASA Goddard's Coordinated Data Analysis Web.7 CINDI data are available through the William B. Hanson Center for Space Science8 at the University of Texas at Dallas.
"Trajectory: C/NOFS (2008-017A) CINDI". NASA. 28 October 2021. Retrieved 20 December 2021. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/spacecraft/displayTrajectory.action?id=2008-017A ↩
"Experiment: C/NOFS Occultation Receiver for Ionospheric Sensing and Specification (CORISS)". NASA. 28 October 2021. Retrieved 19 November 2021. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=2008-017A-04 ↩
"Experiment: Coherent Electromagnetic Radio Tomography (CERTO)". NASA. 28 October 2021. Retrieved 19 November 2021. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=2008-017A-05 ↩
"Experiment: Coupled Ion-Neutral Dynamics Investigation (CINDI)". NASA. 28 October 2021. Retrieved 19 November 2021. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=2008-017A-03 ↩
"Experiment: Planar Langmuir Probe (PLP)". NASA. 28 October 2021. Retrieved 19 November 2021. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=2008-017A-01 ↩
"Experiment: Vector Electric Field Instrument (VEFI)". NASA. 28 October 2021. Retrieved 19 November 2021. This article incorporates text from this source, which is in the public domain. https://nssdc.gsfc.nasa.gov/nmc/experiment/display.action?id=2008-017A-02 ↩
CDAWeb This article incorporates text from this source, which is in the public domain. https://web.archive.org/web/20111008115124/http://cdaweb.gsfc.nasa.gov/cnofs/ ↩
"Home | CINDI Education". cindispace.utdallas.edu. https://cindispace.utdallas.edu/ ↩
"C/NOFS Satellite Successful LEO Operations". USAF. Archived from the original on 18 June 2008. This article incorporates text from this source, which is in the public domain. https://www.losangeles.spaceforce.mil/?id=123100460 ↩
"SpaceDev hardware successfully operates aboard C/NOFS mission". SpaceDev. 9 June 2008. Archived from the original on 15 June 2008. Retrieved 9 June 2008. https://web.archive.org/web/20080615184538/http://www.spacedev.com/press_more_info.php?id=244 ↩
"Communication/Navigation Outage Forecasting System (C/NOFS) On-Orbit Contract Extension". FedBizOps.gov. This article incorporates text from this source, which is in the public domain. https://www.fbo.gov/?s=opportunity&mode=form&id=99017504bfd5e796bee8678d426e0555&tab=core&_cview=0 ↩
"Satellite's Last Days Improve Orbital Decay Predictions". NASA. 14 December 2015. Retrieved 15 December 2015. This article incorporates text from this source, which is in the public domain. https://www.nasa.gov/press-release/goddard/plunging-into-the-ionosphere-satellite-s-last-days-improve-orbital-decay-predictions ↩