SPAD A.2

infobox Aircraft
name = SPAD A.2
type = Fighter

manufacturer = Société Pour l'Aviation et ses Dérivés (SPAD)



caption =
designer = Louis Béchereau
first flight = May 1915
introduction =
retired =
status =
primary user = Russia
more users = France
produced =
number built = 99
unit cost =
developed from = SPAD A.1
variants with their own articles =

The SPAD A.2 (also called SA.2, A-2 or A2) was a French tractor biplane of 1915 that saw some service with France and Russia in the early stages of World War I in the fighter-reconnaissance role.

Design and Development

PAD A.1 prototype

The first military airplane produced by SPAD's chief designer, Louis Béchereau, was the SPAD A.1 prototype. Early combat experience had shown it was desirable to have forward-firing machine guns. However, synchronization devices to fire a gun through the propeller were not yet available and several solutions were tested by various manufacturers. One of the most complex was that adopted by Béchereau on the A.1. In addition to its pilot, the aircraft was designed to carry an observer/gunner placed in a streamlined nacelle in front of the propeller. With this configuration - designed to combine the advantages of the tractor and the pusher types, the observer had a clear field of fire and vision to the front. However, this also seriously limited the pilot's vision, notably during landing, made communication between the pilot and the observer nearly impossible and implied the risk of the observer being hit by the propeller, not to mention being crushed by the motor in even a relatively mild crash or "nose-over". A broadly similar adaptation of the British BE.2c - the BE.9 was abandoned for these reasons.

The nacelle (called a "pulpit") was fitted with a flexible Lewis machine gun on a tubular mount, and incorporated air intakes on its sides to redirect some air towards the 80-hp Le Rhône 9C rotary engine, which was largely screened by the nacelle. It could also be hinged down to give an easier access to the engine or to start it. A wire mesh screen was installed behind the observer, to stop him from hitting the propeller.

Aside from this unorthodox configuration, the aircraft was of a rather standard wood and fabric construction. The wings had a one-bay design. To prevent the long wires from vibrating excessively in flight, two vertical struts were added in the middle of the bay to retain and strengthen the wires, giving the aircraft the looks of a two-bay biplane. The fuselage was reportedly strong and well-designed.

First flight of the A.1 took place in May 1915. The aircraft reached a top speed of 95 mph (153 km/h).

PAD A.2

The SPAD A.2 was an improved version of the A.1 which first flew on 21 May 1915 and later went into production. A total of 99 were produced (42 for France and 57 for Russia). Its flight characteristics were still disappointing and the aircraft was not well-loved by its crews. In spite of this lack of success, the design brought valuable experience to Béchereau and his team and some features, notably the one-bay wing with intermediate struts, were to be used later by Béchereau for the SPAD S.5, which would lead to the extremely successful S.VII and S.XIII fighters.

Russian models were modified to use skis instead of the undercarriage for winter operations.

Variants

*The SPAD A.3 was a dual-control trainer variant of the A.2, with the pilot also being supplied with a gun mount according to some sources. No production followed.
*The SPAD A.4 was an A.2 with a more powerful 110-hp Le Rhône 9J engine. Some 10 were produced and sold to Russia.
*The SPAD A.5 was a (three-seater?) variant powered by a 220-hp Renault 8Fg engine. This variant did not see any production either

Operational History

The A.2 had a short and inauspicious career in the French "Aviation Militaire". Its crews did not appreciate it and it was quickly replaced in service by better types as the introduction of synchronizing gear rendered the entire concept of the A.2 obsolete. Few details are available concerning its career.

The Imperial Russian Air Service was the other user of the SPAD A.2 and kept it in service for a much longer time, due to a shortage in available aircraft on the Eastern front. Although Russian crews also thought very little of the SPAD, at least one crew was successful with it. On November 25, 1916, Russian pilot Karpov and his observer Bratolyubovym shot down a German aircraft near the village of Vulka.

Operators

;FRA;RUS

pecifications (A.2)

aircraft specifications

plane or copter?=plane
jet or prop?=prop

crew= one pilot, one gunner/observer
capacity=
length main= 7.30 m
length alt= 23 ft 11 in
span main= 9.55 m
span alt= 31 ft 4 in
height main= 2.65 m
height alt= 8 ft 8 in
area main= 24.56 m²
area alt= 264.36 ft²
airfoil=
empty weight main= 435 kg
empty weight alt= 958 lb
loaded weight main= 735 kg
loaded weight alt= 1,618 lb
useful load main= kg
useful load alt= kg
max takeoff weight main= kg
max takeoff weight alt= lb
more general=

engine (prop)= 1 x Le Rhône 9C rotary
type of prop=
number of props=
power main=
power alt= 80 hp
power original=

max speed main= 153 km/h
max speed alt= 95 mph
cruise speed main=
cruise speed alt=
stall speed main=
stall speed alt=
never exceed speed main=
never exceed speed alt=
range main= 300 km
range alt= 186 mi
ceiling main= 4300 m
ceiling alt= 14,100 ft
climb rate main= 2000 m (6,560 ft) in 12 min 30 sec
climb rate alt=
loading main=
loading alt=
thrust/weight=
power/mass main=
power/mass alt=
more performance=

armament= 1 .303 Lewis machine gun on a flexible mount

avionics=

References

Book Sources
*cite book
last = Bordes
first = Gérard
title = Mach 1, Encyclopédie de l'Aviation, Vol. 8
publisher = Editions Atlas
year = 1981
isbn =
*cite book
last = Connors
first = John F.
title = SPAD Fighters in action
publisher = Squadron/Signal
year = 1989
isbn = 0-89747-217-9

Websites
*cite web |url=http://www.aviafrance.com/aviafrance1.php?ID=2433&ID_CONSTRUCTEUR=1231&ANNEE=0&ID_MISSION=0&MOTCLEF= |title=aviafrance.com |accessdate=2007-10-01 |format= |work=