Airplanes
WW1 Airplane Markings
During World War One, aircraft markings not only served to differentiate between allied and enemy planes, but also had considerable symbolic importance. The British roundel and the German Iron Cross, for example, were symbols of national pride and identity. Painting an emblem on the fuselage or wings of an aircraft was a common way to show pride in the unit's history and heritage. It was common for these badges to feature the squadron's mascot, insignia of the home city or country, or references to pivotal moments in the unit's history. Pilots' names or nicknames were painted on their planes to help others recognize them and improve morale. Several pilots put unique touches on their planes by painting pinup beauties, cartoon creatures, or animals on the wings. Ultimately, these marks helped improve morale, establish a feeling of identity, and better coordinate military activities for the pilots and their groups.
Germany
General characteristics
Crew: 1
Length: 5.7m (18 ft 8½ in)
Wingspan: 8.35 m (27 ft 7⅞ in)
Height: 2.72 m (8 ft 11 in)
Wing area: 15.1 m² (163 ft²)
Empty weight: 540 kg (1,190 lb)
Loaded weight: 735 kg (1,620 lb)
Powerplant: 1 × Siemens-Halske Sh.III 11-cylinder geared rotary engine, 118 kW (160 PS)
Performance
Maximum speed: 190 km/h (103 knots, 119 mph)
Service ceiling: 8,000 m (26,200 ft)
Wing loading: 48.7 kg/m² (9.94 lb/ft²)
Power/mass: 0.16 kW/kg (0.099 PS/lb)
Endurance: 2 hours
Climb to 1,000 m (3,300 ft): 1.9 min
Climb to 6,000 m (19,700 ft): 15.5 min
Armament
2 × 7.92 mm (0.31 in) LMG 08/15 machine guns
Siemens-Schuckert
Meanwhile, the short-span D.IIc prototype had been improved upon, and its performance had increased substantially thanks to the use of narrower-chord upper and lower wings based on the Göttingen 180 airfoil, each measuring 1.00 meters from leading to trailing edge. In March of 1918, the D.IV was ordered for the first time. Demand increased quickly afterward as people saw the benefits of this new design. Aircraft began arriving at combat units in August, but only 123 of the 280 ordered were completed before war's conclusion, with only half of those making it to active duty. It was officially deemed superior to all other single-seaters in October 1918.
Although landing was difficult due to the plane's tiny landing gear and little prop clearance, flying the plane was a breeze. It was faster and more maneuverable than the Fokker D.VII at altitudes more than 4,000 meters (13,100 feet), and it had a relatively short take-off run. Most notably, it could ascend to an altitude of 6,000 meters (19,700 feet) in less than 14 minutes and had a very high service ceiling. It could climb to 26,600 feet (8,100 meters) in 36 minutes, 1,200 meters (3,900 feet) higher than the Fokker's ceiling. After the armistice, many D.IVs were sold to Switzerland, where they remained in service until the late 1920s. The aircraft division of SSW was disbanded after Germany's aircraft production was banned by the Treaty of Versailles. The Siemens-Halske division survived and eventually morphed into Bramo.
General characteristics
Crew: 1
Length: 7.2 m (23 ft 7 in)
Wingspan: 9.52 m (31 ft 3 in)
Height: 2.4 m (7 ft 10 in)
Wing area: 16 m2 (170 sq ft)
Empty weight: 399 kg (880 lb)
Gross weight: 610 kg (1,345 lb)
Powerplant: 1 × Oberursel U.I 9-cyl.air-cooled rotary piston engine, 75 kW (100 hp)
Performance
Maximum speed: 140 km/h (87 mph; 76 kn)
Endurance: 1.5 hours
Service ceiling: 3,600 m (11,810 ft)
Rate of climb: 3.333 m/s (656.1 ft/min)
Time to altitude:
1,000 m (3,281 ft) in 5 minutes
3,000 m (9,843 ft) in 30 minutes
Armament
Guns: 1 × 7.92 mm (0.312 in) LMG 08/15 machine gun offset to starboard, synchronised to fire through the propeller.
Fokker Eindecker
Leutnant Wintgens shot down a French Morane-Saulnier L two-seat "parasol" monoplane on July 1, 1915, while piloting one of the five M.5K/MG production prototypes, 'E.5/15'. E.Is were "assigned" to Feldflieger Abteilungs so that they could protect their fleet of six two-seat reconnaissance biplanes. Three days after his "unconfirmed" victory, Wintgens was the first Eindecker pilot to win an official match.
Timekeeping for Eindecker guns
Oswald Boelcke and Max Immelmann, both members of Feldflieger Abteilung 62, flew the most renowned Eindecker, aircraft E.3/15, an M.5K/MG. Once Fokker gave back his worn-out A.16/15, Leutnant Otto Parschau—the man responsible for introducing the Eindecker—took control of the M.5K/MG E.1/15. Following WWII, Immelmann purchased E.I. 13/15, which was serialized by IdFlieg. In total, Oswald Boelcke took home 19 of a possible 40 Eindecker trophies. As of June 27, 1916, he no longer had any winning Eindecker streaks to speak of. Max Immelmann, a second-place Einstein, came in second. He was responsible for all 15 victories in the E.III before his death in June 1916, when the synchronization device failed and seven rounds hit a single propeller blade, shattering it. The airliner was rocked by intense vibrations. There were 11 winning Eindecker pilots. As pilots of the Eindecker, Boelcke, Immelmann, and Wintgens were awarded the Pour le Mérite, also known as the "Blue Max," for their performance.
In early 1916, the Eindecker's dominance and "Fokker Scourge" were put to an end by pusher aircraft such as the British Airco DH.2, the Royal Aircraft Factory F.E.2 and F.E.8, and the French Nieuport 11. On September 25, 1916, Heurteaux shot down Wintgens in a SPAD S.VII fighter, killing him.
General characteristics
Crew: 3
Length: 12.42 m (40 ft 8 in)
Wingspan: 23.70 m (77 ft 9 in)
Height: 4.5 m (14 ft)
Wing area: 89.5 m² (963.6 ft²)
Empty weight: 2,739 kg (6,039 lb)
Max. takeoff weight: 3,967 kg (8,745 lb)
Powerplant: 2 × Mercedes D.IVa inline engine, 260 hp (191 kW) each
Performance
Maximum speed: 140 km/h (87 mph)
Range: 840 km (522 miles)
Service ceiling: 6,500 m (21,325 ft)
Armament
2 or 3 × 7.92 mm (.312 in) Parabellum MG14 machine guns
Gotha g V
G.Va
A compound tail unit consisting of biplane horizontal stabilizers and twin rudders was tested by Gotthaer in February of 1918. The aircraft's previously subpar directional control on a single engine was much enhanced by the installation of a new tail unit, or Kastensteuerung. This redesigned tail design was included into the G.Va variant, which also had a somewhat shorter nose fuselage and nose landing gear. Kagohl 3 is now known as Bogohl 3, and it received all 25 G.Va aircraft.
G.Vb
Carried more cargo than the G.Va it replaced and had a maximum takeoff weight of 4,550 kilograms (10,030 lb). Gothaer installed the Stossfahrgestell (German for "shock landing gear"), a tandem two-bogie main landing gear, to lessen the possibility of a nose-over while landing. After the success of the Stossfahrgestell, all G.Vs in Bogohl 3 were required to have one installed. Flettner servo tabs were installed on the ailerons of some G.Vb aircraft as another means of lightening the load required to fly the plane.
Idflieg placed an order for 80 G.Vb planes, the first of which arrived at Bogohl 3 in June of 1918. All eighty planes were completed before the time of the armistice, but the final batch was sent straight to the Allied special commission instead of the front lines.
British
General characteristics
Crew: 2 (pilot & observer/gunner)
Length: 25 ft 10 in (7.87 m)
Wingspan: 39 ft 3 in (11.96 m)
Height: 9 ft 9 in (2.97 m)
Wing area: 405 ft² (37.62 m²)
Empty weight: 2,145 lb (975 kg)
Max. takeoff weight: 3,243 lb (1,474 kg)
Powerplant: 1 × Rolls-Royce Falcon III liquid-cooled V12 engine, 275 hp (205 kW)
Performance
Maximum speed: 123 mph (107 kn, 198 km/h) at 5,000 ft (1,500 m)
Range: 369 mi (320 nmi, 593 km)
Service ceiling: 18,000 ft (5,500 m)
Rate of climb: 889 ft/min (4.5 m/s)
Armament
Guns:
1× .303 in (7.7 mm) forward-firing Vickers machine gun in the upper fuselage
1 or 2× .303 in Lewis Guns in the observer's cockpit
Bombs: 240 lb (110 kg)
bristol type 22
Aircrews were directed to maintain formation and utilize the observers' weapons to engage enemy jets when deployed. The F.E.2b functioned nicely with this typical method. The Bristol's tactics failed at first contact. The British began the Battle of Arras in April 1917 with the F.2A. The first F.2A patrol of six aircraft from No. 48 Squadron RFC, led by Victoria Cross recipient William Leefe Robinson, encountered five Albatros D.IIIs from Jasta 11 under Manfred von Richthofen. Four F.2As were shot down, including Robinson, who was captured.
The updated Bristol showed itself in air-to-air combat with more flexible, aggressive tactics. The type was quick and maneuverable enough to be flown in battle like a single-seat fighter, with the pilot's fixed forward-firing gun as the main weapon and the observer's flexible gun as a "sting in the tail". This way, the Bristol Fighter could defeat any German single-seater.
By the end of World War I, the Royal Air Force possessed 1,583 F.2Bs, ordered in September and October 1917. Bristol, Standard Motors, Armstrong Whitworth, and the Cunard Steamship Company manufactured 5,329 aircraft. After the war, F.2Bs were used in army cooperation and light bombing across the British Empire, especially in the Middle East, India, and China. The New Zealand Permanent Air Force, RAAF, Belgium, Canada, Ireland, Greece, Mexico, Norway, Peru, Spain, and Sweden all used the F.2B. The last "Brisfit" unit, India-based No. 20 Squadron RAF, retired the F.2B in 1932. New Zealand used it for three more years.
Poland ordered 107 Bristol Fighters (105 with Hispano-Suiza 300 hp/220 kW engines, two with RR Falcon III) in 1920, becoming the second largest user. It was Poland's most common aircraft. From July 1920, 40 were deployed for reconnaissance and close air support in the Polish-Soviet war, including the Battle of Warsaw. Post-war, the rest worked. Two were downed by ground fire, one was captured by the Russians, and several crashed. Survivors trained and reconnoitered in Poland until 1932.
General characteristics
Crew: 1
Length: 18 ft 9 in (5.71 m)
Wingspan: 28 ft 0 in (8.53 m)
Height: 8 ft 6 in (2.59 m)
Wing area: 231 ft² (21.46 m²)
Empty weight: 930 lb (420 kg)
Loaded weight: 1,455 lb (660 kg)
Powerplant: 1 × Clerget 9B 9-cylinder Rotary engine, 130 hp (97 kW)
Zero-lift drag coefficient: 0.0378
Drag area: 8.73 square feet (0.811 m2)
Aspect ratio: 4.11
Performance
Maximum speed: 115 mph (185 km/h)
Stall speed: 48 mph (77 km/h)
Range: 300 mi ferry (485 km)
Service ceiling: 21,000 ft (6,400 m)
Rate of climb: 1,085 ft/min (5.5 m/s)
Wing loading: 6.3 lb/ft² (30.8 kg/m²)
Power/mass: 0.09 hp/lb (150 W/kg)
Lift-to-drag ratio: 7.7
Armament
Guns: 2× 0.303 in (7.7 mm) Vickers machine guns
Sopwith Camel
The Royal Flying Corps (RFC) and Royal Naval Air Service (RNAS) deployed the Sopwith Camel during World War I. It is famed for its hump-shaped fuselage and aerial combat capability.
The Sopwith Camel, debuted in June 1917, was a successful fighter plane. Its agility and climbing speed made it a formidable dogfighter. Two synchronized Vickers machine guns fired via the propeller arc in front of the pilot.
Despite its performance, the Sopwith Camel proved difficult to fly. Its powerful rotary engine and forward center of gravity rendered it unstable. Because to its difficulty, the Camel had a high accident rate.
The Sopwith Camel was successful despite its problems. It participated in many of World War I's most memorable aerial engagements and shot down more enemy planes than any other Allied fighter. It remains a legendary fighting plane.
General characteristics
Crew: 4 or 5
Length: 62 ft 10¼ in (19.16 m)
Wingspan: 100 ft (30.48 m)
Height: 22 ft (6.71 m)
Wing area: 1,648 ft² (153.1 m²)
Empty weight: 8,502 lb (3,856 kg)
Max. takeoff weight: 13,360 lb (6,060 kg)
Powerplant: 2 × Rolls-Royce Eagle VIII inline piston, 360 hp (268 kW) each
Performance
Maximum speed: 97.5 mph (84.7 kn, 157 km/h)
Range: 608 nmi (700 mi, 1,120 km)
Service ceiling: 8,500 ft (2,600 m)
Rate of climb: 23 min to 5,000 ft
Endurance: 8 hours
Armament
Guns: 5 × 0.303 in (7.7 mm) Lewis Guns (2 on nose Scarff ring, 2 on dorsal position and 1 at ventral hatch)
Bombs: Up to 2,000 lb (907 kg) of bombs
Handley Page
During World War I, the Royal Air Force (RAF) relied heavily on the Handley Page, a heavy bomber aircraft designed and built in Britain. Among the largest and most powerful aircraft of its day, it helped the Allies immensely by bombing German factories and military installations.
The Handley Page made its debut in 1916 and saw widespread service during the conflict. Its two Rolls-Royce engines propelled it to a top speed of about 97 miles per hour, and its wingspan was more than 100 feet. Each plane had a crew of four to six men, including the pilot, co-pilot, navigator, and gunners.
The Handley Page's primary purpose was bombing, and it could carry up to 2,000 pounds of explosives. It was deployed against a wide range of objectives, including enemy production facilities, storage facilities, and concentrations of troops. The plane was also fitted with cameras for spying on the enemy's whereabouts.
The Handley Page, for all its bulk and weight, was remarkably nimble and capable of extreme maneuvers such as steep dives and rapid spins. Several machine guns were installed all throughout the plane to ward off any aerial attacks.
In the end, the Handley Page proved to be a very useful plane that helped the Allies win World War I. Its reputation as one of the greatest bombers of all time endures because of its ability to strike deep within German territory, a key component in undermining the German war effort.
Accidents and incidents
In 1920, two of the six people on board a Handley Page Transport O/400 that was taking off from the company's airstrip in Cricklewood when it crashed and burned to death after hitting a tree during takeoff.