Glory (satellite)
Encyclopedia
The Glory satellite was a planned NASA
NASA
The National Aeronautics and Space Administration is the agency of the United States government that is responsible for the nation's civilian space program and for aeronautics and aerospace research...

 satellite mission that would have collected data on the chemical, micro-physical and optical properties—and the spatial and temporal distributions—of sulfate
Sulfate
In inorganic chemistry, a sulfate is a salt of sulfuric acid.-Chemical properties:...

 and other aerosol
Aerosol
Technically, an aerosol is a suspension of fine solid particles or liquid droplets in a gas. Examples are clouds, and air pollution such as smog and smoke. In general conversation, aerosol usually refers to an aerosol spray can or the output of such a can...

s, and would have collected solar irradiance
Irradiance
Irradiance is the power of electromagnetic radiation per unit area incident on a surface. Radiant emittance or radiant exitance is the power per unit area radiated by a surface. The SI units for all of these quantities are watts per square meter , while the cgs units are ergs per square centimeter...

 data for the long-term climate record. The science focus areas served by Glory included: atmospheric composition; carbon cycle, ecosystems, and biogeochemistry; climate variability and change; and water and energy cycles. The satellite was lost on March 4, 2011, when its Taurus XL carrier rocket malfunctioned. The cost of the satellite was US$424 million.

Launch

The launch from Vandenberg Air Force Base
Vandenberg Air Force Base
Vandenberg Air Force Base is a United States Air Force Base, located approximately northwest of Lompoc, California. It is under the jurisdiction of the 30th Space Wing, Air Force Space Command ....

, near Lompoc, California
Lompoc, California
Lompoc is a city in Santa Barbara County, California, United States. The city was incorporated in 1888. The population was 42,434 at the 2010 census, up from 41,103 at the 2000 census....

, aboard a Taurus XL
Taurus rocket
Taurus is a four stage, solid fuel launch vehicle built in the United States by Orbital Sciences Corporation. It is based on the air-launched Pegasus rocket from the same manufacturer. The Taurus rocket is able to carry a payload of around 1,350 kg into a low Earth orbit. First launched in 1994,...

 rocket was originally planned for February 23, 2011. It was postponed due to a malfunction in ground support equipment. The next planned date of liftoff
Liftoff
-Plot:Having just been promoted, it's CJ's first day as Chief of Staff. After being introduced to the Secret Service Agents assigned to protect her, it is time for her last press briefing, where she receives a huge round of applause from a stunned Press Room...

 was March 4, 2011. The Taurus rocket also carried three small CubeSat
CubeSat
A CubeSat is a type of miniaturized satellite for space research that usually has a volume of exactly one liter , has a mass of no more than 1.33 kilograms, and typically uses commercial off-the-shelf electronics components...

 satellites built by university students in Montana, Colorado and Kentucky.

The launch took place on March 4, 2011, at 2:09:43 am Pacific Standard Time (10:09:43 UTC) from Vandenberg Air Force Base
Vandenberg Air Force Base
Vandenberg Air Force Base is a United States Air Force Base, located approximately northwest of Lompoc, California. It is under the jurisdiction of the 30th Space Wing, Air Force Space Command ....

. The Taurus XL rocket's first three stages functioned as planned, but the nose cone (also known as the payload fairing
Payload fairing
Payload fairing is one of the main components of a launch vehicle. The fairing protects the payload during the ascent against the impact of the atmosphere . More recently, an additional function is to maintain the cleanroom environment for precision instruments.Outside the atmosphere the fairing is...

) failed to separate 2 minutes 58 seconds after the launch. The nose cone covers and protects the satellite during launch and ascent, and is designed to separate and fall away shortly after the launch. Due to the failure of the nose cone to separate, the rocket remained too heavy to reach the correct orbit. According to launch director Omar Baez, the satellite and launcher probably ended up in the southern Pacific Ocean. The failure was estimated to have cost at least $424 million. This only includes the cost of the satellite itself, and not the cost of the launcher and launch services. During the previous failed Taurus XL launch, the vehicle and services were estimated to have cost $54m.

The previous Taurus XL launch with the Orbiting Carbon Observatory
Orbiting Carbon Observatory
The Orbiting Carbon Observatory 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 February 24, 2009, when the payload fairing of the Taurus rocket which was carrying it failed to...

 (OCO) in February 2009 also ended in a failure due to failed payload fairing separation. Following the failed OCO mission, Taurus XL launches were put on hold for two years as the rocket's manufacturer Orbital Sciences Corporation
Orbital Sciences Corporation
Orbital Sciences Corporation is an American company which specializes in the manufacturing and launch of satellites. Its Launch Systems Group is heavily involved with missile defense launch systems...

 tried to fix the payload fairing separation problem, obviously without success. A British OCO scientist said the loss of Glory was a great blow to the NASA Earth science program, especially since the reason for the launch failure was the same as with OCO.

During a news conference shortly after the launch, Rich Straka from Orbital Sciences Corporation said his company was investigating the failure, noting, "there really isn't enough data to say anything more than the fairing didn't separate."

Scientific instruments

Aerosol Polarimetry Sensor (APS)

The Aerosol Polarimetry Sensor (APS) is a continuous scanning sensor that has the capability to collect visible, near infrared, and short-wave infrared data scattered from aerosols and clouds. It is designed to make multi-angle observations of Earth and atmospheric scene spectral polarization and radiance.

Objectives
  • Determine the global distribution of natural and man-made aerosols (black carbons, sulfates, etc.) with accuracy and coverage sufficient for reliable quantification of: the aerosol effect on climate; the anthropogenic component of the aerosol effect; the potential regional trends in natural and man-made aerosols.
  • Determine the direct impact of aerosols on the radiation budget and its natural and anthropogenic components.
  • Determine the effect of aerosols on clouds (microphysics and coverage) and its natural and anthropogenic components.
  • Determine the feasibility of improved techniques for the measurement of black carbon and dust absorption to provide more accurate estimates of their contribution to the climate forcing.

  • Instrument scientist: Brian Cairns / GSFC (website)
Cloud Camera

The cloud camera is a high-spatial-resolution two-band radiometer intended to facilitate the identification of cloudcontaminated APS pixels and to determine the fraction of the pixel area occupied by clouds. Over ocean, the cloud camera is used to determine aerosol load and fine mode fraction based on the aerosol microphysical model determined from APS measurements. The Cloud Camera is not a separate instrument, rather it is used to identify clouds in the APS nadir pixel.
Total Irradiance Monitor (TIM)

The Total Irradiance Monitor (TIM) is an active cavity radiometer
Radiometer
A radiometer is a device for measuring the radiant flux of electromagnetic radiation. Generally, the term radiometer denotes an infrared radiation detector, yet it also includes detectors operating on any electromagnetic wavelength....

that records total solar irradiance. It has four identical radiometers to provide redundancy and to help detect changes in the instrument from exposure to solar radiation. TIM is mounted on a platform that moves the instrument independent of the spacecraft.

External links

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