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  2. Aero A.101 - Wikipedia

    en.wikipedia.org/wiki/Aero_A.101

    On 23 January 1937, a contract was signed to sell the Spanish Republic all 28 remaining A-101s, together with 24 Letov Š-231 fighters and spare parts, using Estonia as an intermediary. [ 6 ] [ 10 ] [ a ] [ b ] The first batch of A-101s arrived at the port of Gdynia , Poland on 27 February 1937, but did not leave port aboard the Panamanian ...

  3. A101 - Wikipedia

    en.wikipedia.org/wiki/A101

    Download QR code; Print/export Download as PDF; Printable version; In other projects Wikidata item; Appearance. move to sidebar hide. A101 , A.101 or A-101 may refer ...

  4. AgustaWestland AW101 - Wikipedia

    en.wikipedia.org/wiki/AgustaWestland_AW101

    A major agreement, which secured funding for the majority of the EH101's development program, was signed by both the British and Italian governments in 1984. [9] At the 1985 Paris Air Show , Agusta showed a mock-up of a utility version of the new helicopter, leading to a more generalised design that could be customised to meet the needs of ...

  5. OMB Circular A-21 - Wikipedia

    en.wikipedia.org/wiki/OMB_Circular_A-21

    OMB Circular A-21 is a Government circular that sets forth the rules governing the eligibility and calculation of costs in support of sponsored research, development, training and other works produced in agreement with the United States Federal Government, but does not attempt to identify or dictate agency or institutional participation in those works.

  6. Agusta A.101 - Wikipedia

    en.wikipedia.org/wiki/Agusta_A.101

    Data from Jane's All The World's Aircraft 1969–70 General characteristics Crew: 2 Capacity: up to 36 pax / 18 stretchers with 5 attendants / 5,000 kg (11,000 lb) payload Length: 20.19 m (66 ft 3 in) including tail-rotor Width: 4.64 m (15 ft 3 in) rotor blades folded Height: 6.56 m (21 ft 6 in) to top of rotor head Empty weight: 6,850 kg (15,102 lb) Gross weight: 12,400 kg (27,337 lb) Max ...

  7. Pratt & Whitney XA101 - Wikipedia

    en.wikipedia.org/wiki/Pratt_&_Whitney_XA101

    The Pratt & Whitney XA101 is an American adaptive cycle engine demonstrator being developed by Pratt & Whitney for the Lockheed Martin F-35 Lightning II and form the technological foundation for the company's XA103 propulsion system for the United States Air Force's sixth generation fighter program, the Next Generation Air Dominance (NGAD).