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A MS.880B Rallye Club. The SOCATA Rallye is a single-engined, low-wing monoplane light aircraft, capable of STOL (short takeoff and landing) performance. The Rallye is considered to be sound and functional aircraft; efforts were made upon later-built aircraft to improve the type's visual appeal and to clean up the exterior. [19]
MS-GF+ (also known as MSGF+ or MSGFPlus) performs peptide identification by scoring MS/MS spectra against peptides derived from a protein sequence database. MS-GF+ was developed at the Center for Computational Mass Spectrometry at the University of California, San Diego, with later work at Pacific Northwest National Laboratory (PNNL).
Casio fx-115ES scientific calculator with Natural Display. (also called "Natural V.P.A.M." in the updated version) Revised version of the MS Series including the following changes: Multi-line 96×31 dot matrix displays, but character cells are connected by dots like graphing calculators
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MS.732 Prototypes powered by a 200 hp (149 kW) Salmson 8.AS.02 engine and retractable landing gear, [2] two built. MS.733 Production variant with a 240 hp (179 kW) Potez 6D 02 engine, five pre-production and 200 production aircraft built. MS.733A MS.733 gunnery trainers modified for counter-insurgency role; it served from 1955 to 1959.
MS.232 experimental version with 149 kW (200 hp) Clerget 9Ca diesel, 1930. [7] MS.233 powered by 172 kW (230 hp) Gnome-Rhône 5Ba or Gnome-Rhône 5Bc, six built in France and 16 in Portugal under licence for the Portuguese military. [8] MS.234 186 kW (250 hp) Hispano-Suiza 9Qa engine, two built, one for U.S. Ambassador in Paris. [9] MS.234/2
The MS.250 was a parasol-wing monoplane with swept-back wings, similar to the Morane-Saulnier MS.230, but differed in having a new tail. The cockpits had windscreens, and the rear cockpit had a gun ring. The pilot-instructor manned the front cockpit, and the trainee observer manned the rear cockpit. [1]
Data from Jane's All The World's Aircraft 1961–62 General characteristics Crew: 2 Capacity: 2 passengers Length: 10.05 m (33 ft 0 in) Wingspan: 10.15 m (33 ft 4 in) (over tip tanks) Height: 2.60 m (8 ft 6 in) Wing area: 18.0 m 2 (194 sq ft) Aspect ratio: 5.12:1 Empty weight: 1,945 kg (4,288 lb) Gross weight: 3,470 kg (7,650 lb) Fuel capacity: 245 gallons in main tank, 115 gallons in wing ...