Search results
Results From The WOW.Com Content Network
The TR-106 or low-cost pintle engine (LCPE) was a developmental rocket engine designed by TRW under the Space Launch Initiative to reduce the cost of launch services and space flight. Operating on LOX / LH2 the engine had a thrust of 2892 kN, or 650,000 pounds, making it one of the most powerful engines ever constructed.
TRW Inc. was an American corporation involved in a variety of businesses, mainly aerospace, electronics, automotive, and credit reporting. [2] It was a pioneer in multiple fields including electronic components, integrated circuits, computers, software and systems engineering.
TRW Automotive was an American company based in Livonia, Michigan.Tracing its roots from TRW Inc., [2] [3] TRW Automotive's production featured a variety of automotive products including integrated vehicle control and driver assist systems, braking systems, steering systems, suspension systems, seat belts and airbags, and engine valves among others. [4]
A crosshead as part of a reciprocating piston and slider-crank linkage mechanism. Cylindrical trunk guide Hudswell Clarke Nunlow; crosshead and two slide bars. In mechanical engineering, a crosshead [1] is a mechanical joint used as part of the slider-crank linkages of long stroke reciprocating engines (either internal combustion or steam) and reciprocating compressors [2] to eliminate ...
Another view of the engine Close up view on cylinder. The Kharkiv model V-2 (Russian: В-2) is a Soviet diesel tank V-12 engine, the V angle at 60°, with dual overhead camshafts per bank, four valves per cylinder opened by bucket-style followers and direct fuel injection.
The pre-war engines were Glow Head Engines in countless varieties. The first diesel engines were produced in 1938, when the company had 190 employees and an annual production of 160 engines. [2] The engines earned a reputation for being easy to operate and maintain. An engineer once stated that Wichmann were built for morons, but built by ...
The engine made 10 flights during the Apollo program and 77 during its Delta career between 1974 and 1988. The TRW TR-201 was re-configured as a fixed-thrust version of the LMDE for Delta's stage 2. Multi-start operation is adjustable up to 55.6 kN and propellant throughput up to 7,711 kg; and the engine can be adapted to optional expansion ...
The engine has the same stroke as all other redblocks, the smaller displacement is the result of a smaller bore at 88.9 mm × 80 mm (3.50 in × 3.15 in). It is a very robust engine with forged pistons (made by Kolbenschmidt). [citation needed] The B19 later evolved into the B200 low friction engine.