The Cyclone Global Navigation Satellite System (CYGNSS) is intended to probe the inner core of hurricanes to learn about the rapid intensification. Consisting of a constellation of eight microsatellite observatories, the system will be placed at the Low Earth Orbit (LEO) approximately 510km above the surface at an inclination of 35° from the equator.

CYGNSS is being developed by NASA as part of its Earth system science pathfinder programme launched in June 2012, in association with the University of Michigan, and Southwest Research Institute (SwRI).

It is scheduled to be launched from Cape Canaveral Air Force Station in Florida, US, aboard Pegasus XL rocket in December 2016.

Design and development of CYGNSS

CYGNSS consists of eight micro satellites, each weighing roughly 29kg (64lbs) and equipped with four GPS receivers. Each satellite has external dimensions of 51cm x 64cm x 28cm. The structure of the spacecraft integrates microsatellite and instrument electronic boards.

CYGNSS will carry a Delay Doppler Mapping Instrument (DDMI) including a Delay Mapping Receiver (DMR) with two nadir-pointing antennae and one zenith-pointing antenna. It is designed for a lifespan of approximately two years.

Detailed design of the satellite was completed by January 2015. The assembling of eight microsatellites began in August 2015 and completed in February 2016. The functional and environmental testing of the satellites was completed in August 2016 and the system was transported to Vandenberg Air Force Base for integration with Orbital ATK Pegasus XL launch vehicle in August 2016.

The University of Michigan was selected to provide CYGNSS mission design and implementation including the design of the constellation and production of retrieved surface wind speed estimates. The design for CYGNSS was completed at Science Operations Centre located at the University of Michigan.

Southwest Research Institute (SwRI) was selected to construct and test each of the eight CYGNSS microsatellite observatories at its Mission Operations Center. SwRI will also be responsible to offer risk management, systems engineering and mission assurance for CYGNSS.

Surrey Satellite Technology was contracted to design, manufacture and test the Delay Doppler Mapping Instrument (DDMI), a science payload integrated on each CYGNSS microsatellite observatory. The company also provided GPS receivers and other antennae for the CYGNSS satellites.

The deployment module for CYGNSS was provided by Sierra Nevada Corporation.

CYGNSS mission details

“The University of Michigan was selected to provide CYGNSS mission design and implementation including the design of the constellation and production of retrieved surface wind speed estimates.”

The objective of the CYGNSS will be to understand how the ocean surface properties, moist atmospheric thermodynamics, radiation and convective dynamics interact to control the development of a tropical cyclone.

CYGNSS observatories will receive both direct and reflected signals from four independent transmitters in the operational GPS network and will measure surface winds in and near the inner core of hurricanes. Each satellite observatory will be able to measure four simultaneous reflections, which will result in 32 wind measurements a second across the globe.

The constellation of eight satellites will provide gap-free Earth coverage. The observatories will have a median revisit time of three hours and a mean time of seven hours over the critical latitude band for tropical cyclone formation.

Launch vehicle details

Orbital Sciences Corporation was awarded a contract to launch the CYGNSS multi-satellite mission aboard a Pegasus XL rocket in April 2014.

The small space launch vehicle will launch the satellites into LEO orbit using the patented air-launch system located below Orbital’s “Stargazer” L-1011 carrier aircraft over the ocean. The rocket will place the CYGNSS in LEO orbit in a three-staged launch.