C/NOFS

C/NOFS

An artist's concept of C/NOFS
Mission type Technology
Operator STP
AFRL
DMSG
COSPAR ID 2008-017A
Spacecraft properties
Manufacturer General Dynamics
Launch mass 395 kilograms (871 lb)
Start of mission
Launch date 16 April 2008, 17:02:48 UTC
Rocket Pegasus-XL
Launch site Stargazer
Bucholz Runway 6/24
Orbital parameters
Reference system Geocentric
Regime Low Earth
Eccentricity 0.032
Perigee 405 kilometers (252 mi)
Apogee 853 kilometers (530 mi)
Inclination 13.0& degrees
Period 97.3 minutes

C/NOFS, or Communications/Navigation Outage Forecasting System is a satellite developed by the Air Force Research Laboratory Space Vehicles Directorate to investigate and forecast scintillations in the Earth's ionosphere. It was launched by an Orbital Sciences Corporation Pegasus-XL rocket at 17:01 GMT on 16 April 2008.

The satellite, which will be operated by the USAF STP, will allow the US military to predict the effects of ionospheric activity on signals from communication and navigation satellites, outages of which could potentially cause problems in battlefield situations.

C/NOFS has a three-axis stabilisation system, and is equipped with seven sensors. It was placed into a low Earth orbit with orbital inclination of 13°, a perigee of 400 km and an apogee of 850 km. It carries the CINDI experiment for NASA. Launch was originally scheduled for 2003, but was delayed due to a number of issues.

Scientific instruments on board

The spacecraft payload consists of the following instruments:

Scientific Data

C/NOFS science data is now available online for general use. VEFI and PLP data are available through NASA Goddard's Coordinated Data Analysis Web (CDAWeb). CINDI data are available through the William B. Hanson Center for Space Science at The University of Texas at Dallas.

Current status

On 2008-05-28 the USAF Space Development and Test Wing announced its launch and early orbit portion of the spacecraft's operations had been completed successfully.[1] On 2008-06-09 the manufacturer of the separation systems used to deploy the C/NOFS solar panels, payload antennas and magnetometer boom indicated they had all functioned correctly.[2]

On September 9, 2011 SMC announced that it had extended the C/NOFS satellite maintenance contract from 1 October 2011 to 31 March 2012 to Orbital Sciences corp. for the continued On-Orbit Support of the C/NOFS mission.[3]

As of 2013-06-03 the C/NOFS satellite has been placed in safe mode, with all scientific instruments turned off, due to budgetary restrictions.

As of 2013-10-21 the C/NOFS satellite is out of safe mode and operating nominally.

C/NOFS Related Publications

References

External links