If you are looking for information about "Inertial Upper Stage": the following search results will help you to find out what Inertial Upper Stage means.
| 1 | Titan IV |
| -propellant engine. Optional upper stages include the Centaur and inertial upper stage. Guidance...). Optional Centaur upper stage provides 33,100 pounds force (147 kN) and the inertial upper stage provides... low-earth polar orbit when launched from Vandenberg AFB. Using an inertial upper stage, the Titan ... | |
| 2 | STS-44 |
| . Launch set for November 19 delayed due to malfunctioning redundant inertial measurement unit on Inertial Upper Stage booster attached to Defense Support Program satellite. Unit replaced and tested... Inertial Upper Stage (IUS), deployed on flight day one. Cargo bay and middeck payloads: Interim ... | |
| 3 | STS-51-C |
| to Department of Defense. U.S. Air Force Inertial Upper Stage (IUS) booster deployed and met mission... its operating orbit by an Inertial Upper Stage (IUS) booster according to an Air Force announcement... and boosted into its operating orbit by an Inertial Upper Stage (IUS) booster according to an Air ... | |
| 4 | RL-10 (rocket engine) |
| engines are used in the Centaur upper stages of Atlas and Titan rockets. There were proposals to use RL-10 powered Centaur upper stages on Saturn I, Saturn IB and Saturn V rockets. Original RL-10... I / S-IV 2nd stage - 6-engines Vehicle Application: Centaur upper stage - 2-engines ... | |
| 5 | Titan 23B |
| vehicle with an Agena D upper stage added. Primary function: Launch vehicle used to lift medium...) Stages 3 1 - 1st Stage Engines LR87-AJ-5 Thrust 430,000 lb f (1,913 kN) Burn time 147 seconds Fuels A-50 hydrazine/N204 2 - 2nd Stage Engine LR91-AJ-5 Thrust 100,000 lb f (445 kN ... | |
| 6 | J-2 (rocket engine) |
| S-II second stage of the Saturn V rocket. One J-2 engine was used in the Saturn V third stage (S-IVB) and the Saturn IB second stage (S-IVB). There were proposals to use various numbers of J-2 engines in the upper stages of the Nova rocket. Original J-2 Specifications Thrust (altitude): 200,000 lbf ... | |
| 7 | Boeing Integrated Defense Systems |
| launch and exploration X-20 Dyna-Soar X-40 Saturn V Crew Return Vehicle Inertial Upper Stage... Global Observation Satellite GPS Satellites (Rockwell) Integrated Solar Upper Stage Kinetic Energy Anti ... | |
| 8 | STS-33 |
| and boosted into its operating orbit by an Inertial Upper Stage (IUS) booster according to an Air... Mission Parameters Mass: Payload: Magnum ELINT satellite ~ 3,000 kg Booster: IUS upper stage ... | |
| 9 | Multistage rocket |
| the upper stages can use engines suited to near vacuum conditions. Lower stages tend to require more structure than upper as they need to bear their own weight plus that of the stages above them... or more stages as they become empty. (Generally a stage consists of one or more engines, plus fuel ... | |
| 10 | STS-29 |
| Satellite (TDRS-D), which became TDRS-4 in space, and its attached Inertial Upper Stage (IUS), were..., Tracking and Data Relay Satellite-4 (TDRS-4) attached to an Inertial Upper Stage (IUS), became... nearly two hours because of ground fog and high upper winds. A waiver was approved for orbiter wing loads ... | |
| 11 | Saturn (rocket family) |
| , hydrogen-burning upper stages for the Saturn, and outlined eight different configurations for heavy-lift... relied on hardware that had not been developed yet, including the proposed new upper stage. The... I) as a test vehicle, since its lower stage was based on existing technology and its upper stage ... | |
| 12 | STS-26 |
| and Experiments. TDRS-C, which became TDRS-3 in orbit, and its attached Inertial Upper Stage (IUS), were deployed from Discovery's cargo bay 6 hours, 13 minutes, into the flight. The first stage of... Inertial Upper Stage (IUS), became second TDRS deployed. After deployment, IUS propelled satellite to ... | |
| 13 | NERVA |
| -Flight-Test) nuclear stage to be launched in the early 1970s. NERVA was to be a nuclear powered upper stage for the Saturn V. It was to be used to launch interplanetary payloads. NASA's Marshall Space Flight Center had the development responsibility for the rocket stage. The program was cancelled in ... | |
| 14 | Falcon I |
| engine and the upper stage includes one Kestrel engine. The Falcon I is designed to minimize price per... (27,200 kg) Thrust on Liftoff: 71,500 lbf (318 kN) Engines: 1 lower stage Merlin engine; 1 upper stage... Falcon I SpaceX Falcon I. Stages 2 1 - 1st Stage Engines 1 * Merlin engine Thrust ? kN ... | |
| 15 | Titan III |
| . The vehicle is flexible in that it can be launched with no upper stage, or one of two optional upper stages for greater and varied carrying ability. The Titan IIIC consists of a liquid-fueled core... Transtage, was a restartable upper stage used with the Titan IIIA, Titan IIC and Titna 34D. The ... |