The control system for the X-33 linear aerospike engine

IEEE Aerospace Conference Proceedings

Volumn 3, Issue , 1998, Pages 181-191

  Jackson, Jerry E ^a   Espenschied, Erich ^a   Klop, Jeffrey ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; ELECTROMECHANICAL ACTUATORS; ELECTROMECHANICAL DEVICES; FLIGHT CONTROL SYSTEMS; HYPERSONIC AERODYNAMICS; AEROSPACE ENGINEERING; CONTROL SYSTEM ANALYSIS; TRAJECTORIES;

ALTITUDE COMPENSATION; CONVENTIONAL APPROACH; ENGINE CONTROL SYSTEM; FLIGHT TRAJECTORY; PERFORMANCE REQUIREMENTS; SINGLE STAGE TO ORBITS; THRUST VECTOR CONTROL; VEHICLE STRUCTURES;

ENGINES; ROCKET ENGINES;

LINEAR AEROSPIKE ENGINES; SINGLE STAGE TO ORBIT (SSTO); THRUST VECTOR CONTROL (TVC);

EID: 0031621309     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.1998.685796     Document Type: Conference Paper

References (1)

1. XRS-2200 Engine Baseline Description Document (RD97-260), Oct. IO 1997.