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Instruments of Nimbus 1. Nimbus 1 was launched on August 28, 1964, by a Thor-Agena rocket from Vandenberg Air Force Base, California, United States. The spacecraft functioned nominally until September 22, 1964. It re-entered Earth's atmosphere on May 16, 1974. The satellite orbited the Earth once every 1 hour and 38 minutes, at an inclination ...
The Nimbus engines were produced in two main variants, the Mark 103/503 and the Mark 105/502. The Mark 103/503 is generally similar to the Mark 105/502 except that the former has a double-caliper disc brake incorporated in the output drive shaft to provide adequate braking of the helicopter's rotor in the high winds encountered over the deck of a fast moving ship, whereas the 105/502 has a ...
ISO 13216 part 1 (covering lower anchorage points) was published in 1999. Part 2, covering top tether anchorages was published in December 2004. [6] [7]Amendments to include Isofix in United Nations Economic Commission for Europe (UNECE) vehicle regulations 14 and 44, which specify uniform provisions for the design of vehicle seat anchorages and child safety seats, came into force for ...
The Grandis was launched on 14 May 2003 and sold in Japan, Asia, Europe, Oceania, Mexico, Honduras, Jamaica and South America. [1]The exterior styling was based loosely on designer Olivier Boulay's earlier Mitsubishi Space Liner, [2] a monobox four-seat concept vehicle with centre opening "suicide doors", first exhibited at the Tokyo Motor Show in October 2001.
The Mitchell Nimbus is a series of American, single-seat, high-wing gliders that was designed by Don Mitchell in the 1950s. Mitchell is also well known for his ultralight Mitchell Wing A-10 and U-2 designs.
The Albion Nimbus was an underfloor-engined, ultra-lightweight (dry weight 2.4 tonne) midibus or coach chassis, with a four-cylinder horizontal diesel engine and a gross vehicle weight of six tons. It was largely operated on light rural bus duties and private hires.
It was launched in October 1988 at the British International Motor Show and was originally only available with Duple Dartline bodywork. [1] It was 2.3 m (7 ft 7 in) wide and was initially available in the length of 9.0 m (29.5 ft), but later available in lengths of 8.5 m (28 ft) and 9.8 m (32 ft).
The ADC Nimbus was a British inline aero engine that first ran in 1926. The Nimbus was developed from the Siddeley Puma aero engine by Frank Halford of the Aircraft Disposal Company , the goal was to develop the Puma to produce its intended power output which Halford eventually achieved.