She was mission specialist in charge of deploying the Chandra X-ray Observatory and its Inertial Upper Stage out of the shuttle's cargo bay.

Galileo and its Inertial Upper Stage ( IUS ) booster being deployed by the Space Shuttle Atlantis | Space Shuttle Atlantis on the STS-34 mission in October 1989.

New safety protocols introduced as a result of the disaster prohibited the use of the Centaur-G stage on the Shuttle, forcing Galileo to use a lower-powered Inertial Upper Stage solid-fuel booster.

All Mariner-based probes after Mariner 10 used the Titan IIIE, Titan IV unmanned rockets or the Space Shuttle with a solid-fueled Inertial Upper Stage and multiple planetary flybys.

* Carried satellites with a booster, the Payload Assist Module ( PAM-D ) or the Inertial Upper Stage ( IUS ), to the point where the booster sends the satellite to:

Due to velocity change limitations of the Shuttle and the Inertial Upper Stage ( IUS ), this was accomplished by using an encounter with Jupiter to effect the plane change instead of an engine burn.

For the Magellan planetary spacecreft, MSFC managed the adaptation of the Inertial Upper Stage.

Other assignments included the adaptation of the Inertial Upper Stage Booster, a two-stage rocket that would lift Shuttle payloads into higher orbits or interplanetary voyages.

During the mission, Onizuka was responsible for the activities of the primary payloads, which included the unfolding of the Inertial Upper Stage ( IUS ) surface.

Although the TDRS was successfully deployed from Challenger, its two-stage booster rocket, the Inertial Upper Stage ( IUS ), tumbled out of control, placing the satellite into a low elliptical orbit.

At 22, 753 kg, it was the heaviest payload ever launched by the shuttle, a consequence of the two-stage Inertial Upper Stage booster rocket system needed to transport the spacecraft to its high orbit ..

Upper stages, like the Inertial Upper Stage, start and end their productive lives in orbit.

The primary mission objective was accomplished with the successful deployment of a Defense Support Program ( DSP ) satellite with an Inertial Upper Stage ( IUS ) rocket booster.

The primary objective of the STS-93 mission was to deploy the Chandra X-ray Observatory ( formerly the Advanced X-ray Astrophysics Facility ) with its Inertial Upper Stage booster.

Other programs she supported include Space Station, Lunar and Mars Base studies, Inertial Upper Stage, Advanced Orbital Transfer Vehicle, Get-Away Specials, Air Launched Cruise Missile, Minuteman, and Peacekeeper.

The Air Force only stated that the shuttle successfully launched its payload with an Inertial Upper Stage.

The DoD satellite was deployed on the mission's seventh orbit, and successfully boosted into its operating orbit by a U. S. Air Force Inertial Upper Stage ( IUS ) booster.

**: Boeing Inertial Upper Stage

The mission was the second shuttle flight totally dedicated to deploying a Department of Defense payload, after STS-51-C. Its cargo was classified, but it was reported that two ( USA-11 and USA-12 ) DSCS-III ( Defense Satellite Communications System ) satellites were launched into stationary orbits by an Inertial Upper Stage.

TDRS-C, which became TDRS-3 in orbit, and its attached Inertial Upper Stage ( IUS ), were deployed from Discoverys cargo bay six hours and 13 minutes into the flight.

* NASA's Tracking and Data Relay Satellite-3 ( TDRS-3 ), attached to an Inertial Upper Stage ( IUS ), became the second TDRS deployed.

The mission's primary payload was a Tracking and Data Relay Satellite ( TDRS-D ), which became TDRS-4 after deployment, and its attached Inertial Upper Stage ( IUS ).

The primary payload, the Magellan spacecraft with its attached Inertial Upper Stage ( IUS ), was successfully deployed later that day.

The primary payload, the Project Galileo spacecraft with its attached Inertial Upper Stage ( IUS ), was successfully deployed on its journey to Jupiter.

The satellite was deployed on the 7th orbit, and ignited its Inertial Upper Stage ( IUS ) booster at the ascending node of the 8th orbit, successfully placing it in a geosynchronous transfer orbit.

TDRS E, which became TDRS-5 on orbit, was successfully boosted to geosynchronous orbit at more than 22, 000 miles () above Earth by two firings of the Inertial Upper Stage ( IUS ) booster, the last of which occurred approximately 12½ hours into the mission.

A launch set for 19 November was delayed due to replacing and testing a malfunctioning redundant inertial measurement unit on the Inertial Upper Stage booster attached to the Defense Support Program satellite.

It was later successfully transferred to its proper orbit by the Inertial Upper Stage booster.

The deployment operations utilized 3 separate control centers ; the White Sands ground station controlled the TDRS, the JSC Mission Control Center ( MCC ) controlled the shuttle, and the Inertial Upper Stage ( IUS ) control center at Onizuka Air Force Base in Sunnyvale California controlled the booster stage.

The primary mission objective was the deployment of a Defense Support Program ( DSP ) satellite with an Inertial Upper Stage ( IUS ) rocket booster.

Many Tracking and Data Relay Satellites were launched in the 1980s and 1990s with the Space Shuttle and made use of the Inertial Upper Stage, a two-stage solid rocket booster developed for the shuttle.

The mission's primary objective was the deployment of a Defense Support Program satellite with an Inertial Upper Stage booster rocket.

Another DSP satellite was lost in 1999, after its Inertial Upper Stage failed following launch from a Titan 4 booster.

* Inertial Upper Stage, a two-stage solid-fueled booster rocket developed by the U. S. Air Force

Inertial and non-inertial reference frames can be distinguished by the absence or presence of fictitious forces, as explained shortly.

It is an Inertial Guidance System with an additional Star-Sighting system, which is used to correct small position and velocity errors that result from launch condition uncertainties due to the sub navigation system errors and some errors that have accrued by the guidance system during the flight due to imperfect instrument calibration.

* Inertial waves, which occur in rotating fluids and are restored by the Coriolis effect ;

Inertial confinement is used in the hydrogen bomb, where the driver is x-rays created by a fission bomb.

Inertial confinement fusion ( ICF ) is a process where nuclear fusion reactions are initiated by heating and compressing a fuel target, typically in the form of a pellet that most often contains a mixture of deuterium and tritium.

The MEMS-based gyro was initially made practical and producible by Systron Donner Inertial ( SDI ).

The first prototype AIRS, by then known more generically as the Inertial Measurement Unit, or IMU, was delivered in May 1986, 203 days late.

The primary mission was the launch and deployment of the 7th Tracking and Data Relay Satellite ( TDRS ) by means of the two-stage Inertial Upper Stage ( IUS ) solid rocket.

During the four-day mission, the crew successfully deployed the Tracking and Data Relay Satellite ( TDRS-C ), which was subsequently carried to orbit by the Inertial Upper Stage ( IUS ) rocket.

During the four-day mission, the crewmen successfully deployed the Tracking and Data Relay Satellite ( TDRS-C ), which was subsequently carried to orbit by the Inertial Upper Stage ( IUS ) rocket.

* Mach6: Inertial mass is affected by the global distribution of matter.

Modern radars have an integral Inertial Navigation System, often aided by GPS.

Work on a new Fault Tolerant Inertial Navigation Unit ( FTINU ) started in 2001 to enhance mission reliability for Atlas vehicles by replacing the existing non-redundant navigation and computing equipment with a fault tolerant unit.

This has now been replaced by Global Navigation Air Data Inertial Reference System ( GNADIRS ).

Inertial inflation is a concept coined by structuralist inflation theorists.