by National Aeronautics and Space Administration, For sale by the National Technical Information Service in [Washington, DC], [Springfield, Va .
Written in English
|Statement||Ahmet Duyar, Ten-Huei Guo and Walter C. Merrill.|
|Series||NASA technical memorandum -- 101982.|
|Contributions||Guo, Ten-Huei., Merrill, Walter C., United States. National Aeronautics and Space Administration.|
|The Physical Object|
Some authors opted for identifying the system due to its com- plexity, such as , devoted to the staged-combustion SSME (Space Shuttle Main Engine). They considered an . System identification techniques are used to represent the dynamic behavior of the Space Shuttle Main Engine. The transfer function matrices of the linearized models of both the closed loop and the open loop system are obtained by using the recursive maximum likelihood by: 6. Abstract System identification techniques are used to represent the dynamic behavior of the Space Shuttle Main Engine. The transfer function matrices of the linearized models of both the closed loop and the open loop system are obtained by using the recursive maximum likelihood method Topics: SPACECRAFT PROPULSION AND POWER. Books. AIAA Education Series; Library of Flight; Progress in Astronautics and Aeronautics; Identification and control of aircraft dynamics using radial basis function neural networks. Modeling space shuttle main engine using feed-forward neural by: 5.
Space Shuttle Main Engine sensor modeling using radial-basis-function neural networks. Kevin R. Wheeler, ; Atam P. Dhawan and ; Claudia M. MeyerCited by: 5. The Space Shuttle Main Engine (SSME) was designed for 55 missions. The engines were generally referred to as the center (engine 1), left (engine 2), and right (engine 3). The SSMEs were 14 feet long and feet in diameter at the nozzle exit. Each nozzle had an area ratio of Each SSME weighed. Shuttle Test of RS25 Core Stage Engine for Space Launch System Shell Buckling Structural Test Selective Laser Melting Engine Parts Solid Rocket Booster Test Friction Stir Welding for Core Stage MPCV Stage Adapter Assembly RS (SSME) Core Stage Engines in Inventory 70t tFile Size: 5MB. The Aerojet Rocketdyne RS, also known as the Space Shuttle main engine (SSME), is a liquid-fuel cryogenic rocket engine that was used on NASA's Space Shuttle. NASA is planning to continue using the RS on the Space Shuttle's successor, the Space Launch System (SLS).Associated L/V: Space Shuttle, Space Launch System.
The Space Shuttle Main Engine (SSME) (Figure 1) is a high chamber pressure (over 3, pounds per square inch) rocket engine that burns liquid oxygen (LOX) and liquid hydrogenFile Size: KB. Get this from a library! Identification of space shuttle main engine dynamics. [Ahmet Duyar; Ten-Huei Guo; Walter C Merrill; United States. National Aeronautics and Space Administration.]. Well, space shuttle main engines, the SSMEs, there are three of those on each of the orbiters, including Endeavour for STS But then you add the solid rocket boosters and of course the various orbit maneuver engines that round out the propulsion picture on the shuttle. James from Atlanta, Georgia During launch. This paper presents a simplified model of the space shuttle main engine (SSME) dynamics valid within the range of operation of the engine. This model is obtained by linking the linearized point models obtained at 25 different operating points of the by: 2.