goes_nopq2

Next-Generation Weather Satellites

GOES illustration

 

General Characteristics:

 

Customer NOAA, NASA
Washington, D.C.,
Greenbelt, Md.
NOAA, NASA
Washington, D.C.,
Greenbelt, Md.
NOAA, NASA
Washington, D.C.,
Greenbelt, Md.
Spacecraft Modified Boeing 601 Modified Boeing 601 Modified Boeing 601
Launch
Date
Vehicle
Site
GOES-N
May 24, 2006
Delta IV
Cape Canaveral, Fla.
GOES-O
June 27, 2009
Delta IV
Cape Canaveral, Fla.
GOES-P
March 4, 2010
Delta IV
Cape Canaveral, Fla.
Orbital Slots 75° W longitude and 135° W longitude 75° W longitude and 135° W longitude 75° W longitude and 135° W longitude
On-Orbit life 10 years 10 years 10 years

 

Description and Purpose:

The N-P series of Geostationary Operational Environmental Satellites (GOES) comprise the most advanced, next-generation weather satellites ever built and provide the National Oceanic and Atmospheric Administration (NOAA) with enhanced coverage of the entire western hemisphere.

Customer:

In January 1998, Boeing Space and Intelligence Systems of El Segundo, Calif., was awarded a contract from NASA's Goddard Space Flight Center in Greenbelt, Md. The contract currently includes the design, manufacture, integration and launch of three satellites, GOES-N, GOES-O and GOES-P. The GOES program is funded and operated by NOAA. Upon completion of N through P, the company will have built a total of eight spacecraft in the GOES series.

Based on the highly successful Boeing 601 spacecraft, the new satellites will provide more accurate location of severe storms and other weather phenomena, resulting in more precise warnings to the public. The three-axis modified Boeing 601 body-stabilized spacecraft design enables the primary sensors to "stare" at Earth and thus frequently image clouds, monitor Earth's surface temperature, and sound Earth's atmosphere for its vertical temperature and water vapor distribution. Atmospheric phenomena can be tracked, ensuring real-time coverage of short-lived dynamic events, such as severe local storms and tropical hurricanes and cyclones, two types of meteorological events that directly affect public safety, property, and ultimately, economic health and development.

Boeing will furnish the communications subsystem with a search and rescue capability to detect distress signals from ships and airplanes, and will also furnish space environmental monitoring instruments and operator training. Ground station upgrades will be provided by Boeing's teammate Integral Systems Inc. Boeing will also integrate three government-furnished instruments: an Imager and a Sounder built by ITT Industries, Inc., and a Solar X-Ray Imager built by Lockheed Martin.

The imager is a multispectral five-channel instrument that produces visible and infrared images of Earth's surface, oceans, cloud cover and severe storm developments. The multispectral sounder provides vertical temperature and moisture profiles of the atmosphere, augmenting data from the imager. Sounder data are also used in computer models that produce mid- and long-range weather forecasts. A new Solar X-Ray imager will monitor the sun's X-rays for the early detection of solar flares. This early warning is important because these solar flares affect not only the safety of humans in high-altitude missions, such as the Space Shuttle, but also military and commercial satellite communications. The GOES satellites also carry space environment monitoring instruments, built by Panametrics, Inc., which monitor X-rays, extreme ultraviolet and particle emissions including solar protons, alpha particles, and electrons. These space environment monitoring instruments also include a magnetometer, built by Science Applications International Corporation, which samples the Earth's magnetosphere.

A data collection system on GOES receives and relays environmental data sensed by widely dispersed surface platforms such as river and rain gauges, seismometers, tide gauges, buoys, ships, and automatic weather stations. Platforms transmit sensor data to the satellite at regular or self-timed intervals, upon interrogation by the satellite, or in an emergency alarm mode whenever a sensor receives information exceeding a preset level.

Artist rendering of GOES NOPQ satellite shown stowed and deployed.
Stowed (left); In Orbit (right)

Background:

The first Boeing-built GOES satellite, GOES-D, was launched in 1980. This was followed by GOES-E in 1981, GOES-F in 1983, GOES-G in 1986 (booster failed during launch) and GOES-H in 1987. GOES-N, known today as GOES-13, launched on May 24, 2006.

GOES-14, formerly called GOES-O, was handed over to the government on December 14, 2009, following its launch on a Delta IV rocket from Cape Canaveral Air Force Station, Fla., on June 27, 2009.

GOES-P, the last satellite in the N-P series, launched on March 4, 2010, from Cape Canaveral Air Force Station on a Delta IV rocket procured by Boeing Launch Services.

The GOES satellites transmit data collected to NOAA's Wallops, Va., ground station, which relays the data to the NOAA Satellite Operations Control Center in Suitland, Md. The information is then processed and distributed to users throughout the world.

Boeing is the world's leading manufacturer of commercial communications satellites and is also a major provider of space systems, satellites, and payloads for national defense, science and environmental applications.

GOES N-P SPECIFICATIONS

PAYLOAD
S-band 8 downlinks
5 uplinks
L-band 1 downlink
UHF 1 downlink
2 uplinks
POWER
Solar
Beginning of life
End of life
Panels

2.3 kW
2 kW
1 wing, w/1 panel
of dual-junction gallium
arsenide solar cells
Batteries 24-cell NiH2, 123 A-hr
PROPULSION
Liquid apogee motor 110 lbf (490 N)
Stationkeeping thrusters
(bipropellant)

12 x 2 lbf (9 N)
DIMENSIONS
In orbit L, solar array: 26 ft 9 in (8.2 m)
W, antenna: 7 ft 4 in x 11 ft
(2.25 m x 3.37 m)
Stowed H: 12 ft (3.63 m)
W: 7 ft 4 in x 11 ft
(2.25 m x 3.37 m)
Weights
Launch
In orbit
(beginning of life)

7,035 lb (3,199 kg)
4,924 lb (2,238 kg)
ANTENNAS
3 S-band/L-band receive and transit
1 Aft omni antenna
1 UHF, cup-shaped with dipole
2 forward T&C RF horns
LAUNCH VEHICLE COMPATIBILITY
Delta IV Atlas III and V
040233_011/2005/05-05