The Library of Congress > Linked Data Service
 
  Label Dataset Type Subdivision Identifier
1. Thrust reversers

 LC Classification (LCC)
 ClassNumber
Topic		 TL709.5.T5
Technology--Motor vehicles. Aeronautics. Astronautics--Aeronautics. Aeronautical engineering--Jet propulsion. Jet engines--Details and parts of jet engines, A-Z--Thrust reversers ; Thrust reversers--Jet engines
2. Parlett, Lysle P. Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap Washington: National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]; 1970

 BIBFRAME Instances
 Instance 4105121
3. United States. Office of Scientific Research and Development. National Defense Research Committee. condenser gage apparatus for measuring the pressure and thrust characteristics of jet propulsion motors

 BIBFRAME Works
 Work
Text
Multimedia		 21841327
4. United States. Office of Scientific Research and Development. National Defense Research Committee. Large-thrust jet units with 4-second burning time [United States]: [Office of Scientific Research and Development, National Defense Research Committee, Division 8-Explosives]; 11-14-1945

 BIBFRAME Instances
 Instance 21841330
5. United States. Office of Scientific Research and Development. National Defense Research Committee. Characteristics of low-thrust, long-burning jet propulsion units utilizing molded composite propellant [United States]: [Office of Scientific Research and Development, National Defense Research Committee, Division 8-Explosives]; 11-20-1945

 BIBFRAME Instances
 Instance 21841257
6. United States. Office of Scientific Research and Development. National Defense Research Committee. A condenser gage apparatus for measuring the pressure and thrust characteristics of jet propulsion motors [United States]: [Office of Scientific Research and Development, National Defense Research Committee, Division 8-Explosives]; 08-05-1943

 BIBFRAME Instances
 Instance 21841327
7. United States. Office of Scientific Research and Development. National Defense Research Committee. The decipede, a 1000-pound thrust, 43-second burning time, jet propulsion unit [United States]: [Office of Scientific Research and Development, National Defense Research Committee, Division 8-Explosives]; 11-20-1945

 BIBFRAME Instances
 Instance 21841331
8. Parlett, Lysle P. Wind-tunnel investigation of a jet transport airplane configuration with high thrust-weight ratio and an external-flow jet flap

 BIBFRAME Works
 Work
Text
Monograph		 4105121
9. Rowley, R. W. The effect of injector design on thrust-chamber erosion Pasadena: Jet Propulsion Laboratory, California Institute of Technology; 1966

 BIBFRAME Instances
 Instance 4569374
10. Wesseling, P. A two-variable asymptotic solution for three-dimensional, solar-powered, low-thrust trajectories in the vicinity of the ecliptic plane Pasadena: Jet Propulsion Laboratory, California Institute of Technology; 1967

 BIBFRAME Instances
 Instance 4537687
11. Kelly, Arnold James, 1933- Analysis of the interaction of the Surveyor radar altimeter doppler velocity sensor system and vernier thrust chamber plumes Pasadena: Jet Propulsion Laboratory, California Institute of Technology; 1966

 BIBFRAME Instances
 Instance 3602641
12. The decipede, a 1000-pound thrust, 43-second burning time, jet propulsion unit

 BIBFRAME Works
 Work
Text
Monograph
Multimedia		 21841331
13. Large-thrust jet units with 4-second burning time

 BIBFRAME Works
 Work
Text
Monograph
Multimedia		 21841330
14. Characteristics of low-thrust, long-burning jet propulsion units utilizing molded composite propellant

 BIBFRAME Works
 Work
Text
Monograph
Multimedia		 21841257
15. Jet planes--Thrust reversers

 LC Subject Headings (LCSH)
 ComplexSubject
ComplexType
Authority		 sh85070168
Thrust reversers (Jet plane)


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