INTELLIGENCE-SURVEILLANCE-RECONNAISSANCE
Surveil ground targets / target areas to assess environmental threat levels, enemy strength, or enemy movement.
UNMANNED
Aircraft inherently designed (or later developed) with an unmanned capability to cover a variety of over-battlefield roles.
27.2 ft
(8.30 meters)
Length
49.2 ft
(15.00 meters)
Width/Span
1,830 lb
(830 kilograms)
Empty Weight
2,601 lb
(1,180 kilograms)
Maximum Take-Off Weight
+772 lb
(+350 kg)
Weight Difference
monoplane / mid-mounted / straight
Mainplane Arrangement
Monoplane
Design utilizes a single primary wing mainplane; this represents the most popular modern mainplane arrangement.
Mid-Mounted
Mainplanes are mounted along the midway point of the sides of the fuselage.
Straight
The planform involves use of basic, straight mainplane members.
1 x Rotaz 914 engine developing 115 horsepower driving three-bladed propeller unit at the rear of the fuselage in "pusher" configuration.
Propulsion
137 mph
(220 kph | 119 knots)
Max Speed
115 mph
(185 kph | 100 knots)
Cruise Speed
+22 mph
(+35 kph | 19 knots)
Speed Difference
30,003 ft
(9,145 m | 6 miles)
Ceiling
1,553 miles
(2,500 km | 1,350 nm)
Range
1,200 ft/min
(366 m/min)
Rate-of-Climb
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
None. Only mission-specific payloads centered on ISR (Intelligence-Surveillance-Reconnaissance) carried.
Hermes 900 - Base Series Designation.
