I think that a Horsa would be useful both as a static object and for a different type of mission. Plus it would be useful for mission builders
Link to pilots notes including cockpit details
www.keepitsoaring.com/LKSC/Downloads/Horsa_Glider_Notes.pdfThe Horsa Mark I had a wingspan of 88 feet (27 m) and a length of 67 feet (20 m), and when fully loaded weighed 15,250
pounds (6,920 kg).[17]
The Horsa was considered sturdy and very manoeuvrable for a glider. Its design was based on a high-wing cantilever
monoplane with wooden wings and a wooden semi-monocoque fuselage. The fuselage was built in three sections bolted together,
the front section held the pilot's compartment and main freight loading door, the middle section was accommodation for
troops or freight, the rear section supported the tail unit. It had a fixed tricycle landing gear and it was one of the
first gliders equipped with a tricycle undercarriage for take off. On operational flights the main gear could be jettisoned
and landing was then made on the castoring nose wheel and a sprung skid under the fuselage.[18]
The wing carried large "barn door" flaps which, when lowered, made a steep, high rate-of-descent landing possible —
allowing the pilots to land in constricted spaces. The pilot's compartment had two side-by-side seats and dual controls.
Aft of the pilot's compartment was the freight loading door on the port side. The hinged door could also be used as a
loading ramp. The main compartment could accommodate 15 troops on benches along the sides with another access door on the
starboard side. The fuselage joint at the rear end of the main section could be broken on landing to assist in rapid
unloading of troops and equipment. Supply containers could also be fitted under the centre-section of the wing, three on
each side. The later AS 58 Horsa II had a hinged nose section, reinforced floor and double nose wheels to support the extra
weight of vehicles. The tow cable was attached to the nose wheel strut, rather than the dual wing points of the Horsa I
Specifications (AS 51)
Data from British Warplanes of World War II
General characteristics
Crew: 2
Capacity: 25 troops (20-25 troops were the "standard" load)
Length: 67 ft 0 in (20.43 m)
Wingspan: 88 ft 0 in (26.83 m)
Height: 19 ft 6 in (5.95 m)
Wing area: 1,104 ft² (102.6 m²)
Empty weight: 8,370 lb (3,804 kg)
Loaded weight: 15,500 lb (7,045 kg)
Performance
Maximum speed: 150 mph on tow; 100 mph gliding (242 km/h / 160 km/h)
Wing loading: 14.0 lb/ft² (68.7 kg/m²)