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  2. Maule M-7 - Wikipedia

    en.wikipedia.org/wiki/Maule_M-7

    Data from manufacturer and FAA General characteristics Crew: one Capacity: four passengers Length: 23.67 ft (7.21 m) Wingspan: 32.92 ft (10.03 m) Height: 6.33 ft (1.93 m) Empty weight: 1,549 lb (703 kg) typical, equipped Gross weight: 2,500 lb (1,134 kg) Fuel capacity: 40 U.S. gallons (150 L; 33 imp gal) usable (standard) Powerplant: 1 × Lycoming O-540-J1A5D six cylinder, horizontally-opposed ...

  3. Kronshtadt Orion - Wikipedia

    en.wikipedia.org/wiki/Kronshtadt_Orion

    Orion-2 Helios (export version) at MAKS-2021 airshow, Moscow. Main article: Kronshtadt Helios-RLD Helios-RLD is a larger version of the original Orion, with a bigger payload, classified as a high-altitude long-endurance (HALE) UAV, It weighs 5 tonnes (11,000 pounds) with a wingspan of 30 meters (98.42 feet). [ 19 ]

  4. Thiele/Small parameters - Wikipedia

    en.wikipedia.org/wiki/Thiele/Small_parameters

    These parameters are published in specification sheets by driver manufacturers so that designers have a guide in selecting off-the-shelf drivers for loudspeaker designs. Using these parameters, a loudspeaker designer may simulate the position, velocity and acceleration of the diaphragm, the input impedance and the sound output of a system ...

  5. HCCA - Wikipedia

    en.wikipedia.org/wiki/HCCA

    HCCA can stand for: (Hybrid Coordination Function) Controlled Channel Access; α-Cyano-4-hydroxycinnamic acid This page was last edited on 27 ...

  6. List of Lockheed P-3 Orion variants - Wikipedia

    en.wikipedia.org/wiki/List_of_Lockheed_P-3_Orion...

    A Lockheed P-3F Orion of the Islamic Republic of Iran Air Force (s/n 5-8703), at Shiraz Int'l Airport in 2007. Six P-3F Orions delivered to the former Imperial Iranian Air Force in the late 1970s. The airframe of the P-3F was based on the P-3C, which was the then-current production variant of the P-3 for the USN.

  7. Terrier Orion - Wikipedia

    en.wikipedia.org/wiki/Terrier_Orion

    The Terrier Orion system is designed to be rail launched, and can be supported at most fixed and mobile launch sites. [2] The Terrier Mk 12 Mod 1 or Mk 70 rocket used for the first stage uses an 18-inch (46 cm) diameter motor along with 2.5-or-4.8-square-foot (0.23 or 0.45 m 2) cruciform configured tail fins. The Improved Orion motor used in ...

  8. European Service Module - Wikipedia

    en.wikipedia.org/wiki/European_Service_Module

    The "Orion 606" SM design retained the 5-meter (16 ft) width for the attachments of the Orion SM with the Orion CM, but used a Soyuz-like service module design to allow Lockheed Martin to make the vehicle lighter in weight and permitting the attachment of the decagonal solar panels at the module's midpoints, instead of at the base near the ...

  9. Aurora Flight Sciences Orion - Wikipedia

    en.wikipedia.org/wiki/Aurora_Flight_Sciences_Orion

    Work on the Orion began in 2006, when the U.S. Army funded it as a hydrogen-fuelled “high-altitude, long-loiter” (HALL) UAV. Originally, it was conceived as a single-engine, hydrogen-fueled, high-altitude unmanned aircraft intended to carry a 400 lb (180 kg) payload to 65,000 ft (20,000 m) having a 7,000 lb (3,200 kg) gross weight; similar aircraft included the AeroVironment Global ...

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