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  2. StrongARM - Wikipedia

    en.wikipedia.org/wiki/StrongARM

    The StrongARM is a family of computer microprocessors developed by Digital Equipment Corporation and manufactured in the late 1990s which implemented the ARM v4 instruction set architecture. [1] It was later acquired by Intel in 1997 from DEC's own Digital Semiconductor division as part of a settlement of a lawsuit between the two companies ...

  3. List of ARM processors - Wikipedia

    en.wikipedia.org/wiki/List_of_ARM_processors

    ARM further provides a chart [3] ... ARMv3 first to support 32-bit memory address space (previously 26-bit). ... StrongARM ARMv4 SA-110

  4. Comparison of orbital launch systems - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_orbital...

    The following chart shows the number of launch systems developed in each country, and broken down by operational status. Rocket variants are not distinguished; i.e., the Atlas V series is only counted once for all its configurations 401–431, 501–551, 552, and N22.

  5. Digital Equipment Corporation - Wikipedia

    en.wikipedia.org/wiki/Digital_Equipment_Corporation

    Digital Equipment Corporation (DEC / d ɛ k / ⓘ), using the trademark Digital, was a major American company in the computer industry from the 1960s to the 1990s. The company was co-founded by Ken Olsen and Harlan Anderson in 1957.

  6. General Dynamics–Grumman EF-111A Raven - Wikipedia

    en.wikipedia.org/wiki/General_Dynamics–Grumman...

    The aircraft's electrical and cooling systems had to be extensively upgraded to support this equipment. ... Zero-lift drag coefficient: 0.0186 (F ... Marcelle Size ...

  7. Super heavy-lift launch vehicle - Wikipedia

    en.wikipedia.org/wiki/Super_heavy-lift_launch...

    The Shuttle-Derived Heavy Lift Launch Vehicle ("HLV") was an alternate super heavy-lift launch vehicle proposal for the NASA Constellation program, proposed in 2009. [76] A 1962 design proposal, Sea Dragon, called for an enormous 150 m (490 ft) tall, sea-launched rocket capable of lifting 550 t (1,210,000 lb) to low Earth orbit.