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2. G-Shock - Wikipedia

   en.wikipedia.org/wiki/G-Shock

   The GW-M5610 would spawn many variants, the most notable being the GW-5000 which was a steel cased screw-back variant like the original G-Shock but featured diamond like coating (dlc) on the case and caseback and the GW-S5600 which featured Casio's first application of carbon fibre in a watch strap along with the use of titanium in the caseback ...

3. ATA Spec 100/iSpec 2200 - Wikipedia

   en.wikipedia.org/wiki/ATA_Spec_100/iSpec_2200

   ATA Spec 2100 focused on electronic data exchange implemented in SGML. iSpec 2200 was first published in 2000. It incorporates the previous 100 and 2100 specs which won't be maintained beyond their final 1999 revisions.

4. Rolls-Royce AE 2100 - Wikipedia

   en.wikipedia.org/wiki/Rolls-Royce_AE_2100

   The Rolls-Royce AE 2100 is a turboprop developed by Allison Engine Company, now part of Rolls-Royce North America. The engine was originally known as the GMA 2100, when Allison was a division of former corporate parent General Motors .

5. MIL-S-901 - Wikipedia

   en.wikipedia.org/wiki/MIL-S-901

   Motors weighing 250 pounds (110 kg) or less shall be tested on the lightweight shock testing machine. Motors weighing in excess of 250 pounds and up to 6,000 pounds (2,700 kg) shall be tested on a medium weight shock testing machine. Motors weighing over 6,000 pounds shall be tested on a floating shock test platform or barge test.

6. Table of handgun and rifle cartridges - Wikipedia

   en.wikipedia.org/wiki/Table_of_handgun_and_rifle...

   2100 2266 53mm 9×56mm MS 1900 Austria-Hungary 0 R 9×56mm 2100 2400 0.356 56mm Mannlicher–Schönauer 9×57mm Mauser: 1890 Germany R 9.06×56.8mm 2423 [3] 2692 [8] 2.222 46 [3] 0.356 [3] 56.8mm Also available in a rimmed version. [3] 9.3×57mm: 1900 Sweden 1 R 9.3×57mm 2362 2875 0.365 57mm Scandinavian 8×57mm variant currently offered by ...

7. Gulfstream G200 - Wikipedia

   en.wikipedia.org/wiki/Gulfstream_G200

   Data from Frawley Gulfstream G200 data General characteristics Crew: 2 Capacity: Typical Seating of 8-10, 18 Max / 4,050 lb (1,840 kg) Length: 62 ft 3 in (18.97 m) Wingspan: 58 ft 1 in (17.70 m) Height: 21 ft 5 in (6.53 m) Wing area: 369 sq ft (34.3 m 2) Empty weight: 19,200 lb (8,709 kg) Max takeoff weight: 35,450 lb (16,080 kg) Powerplant: 2 × Pratt & Whitney Canada PW306A turbofans, 6,040 ...