Number 22Defense
A publication of the Horizons
DECEMBER 2002Center for Technology and National Security Policy
National Defense University
The Emergence of Mini UAVs for
Military Applications
by Timothy Coffey and John A. Montgomery
Mini UAVs would be more vulnerable to attack and loss due toOverview
their low-altitude missions and could suffer high attrition rates.
The successes of the unmanned aerial vehicle (UAV) in
Thus, they would have to be inexpensive enough to be expendable
Afghanistan most likely will accelerate the introduction of UAVs
while also capable of flying useful payloads. To meet these require-
into the military force structure. What emerged in Afghanistan
ments, we believe that these UAVs would have to be small and elec-
was a tiered observation-detection-targeting system consisting of
trically powered and use mass-produced, commercial off-the-shelf
spacecraft, the Global Hawk UAV, the Predator UAV, and often a
(COTS) technology. Electrically powered motors were chosen for the
spotter on the ground. However, in complex terrain, as in
mini UAVs discussed herein because of their low acoustic signature,
Afghanistan, and in urban situations, airborne assets may be
ease of start, reliability, and relative performance insensitivity to
needed much closer to the ground. A low-altitude tier of UAVs—
altitude and temperature. Although the internal combustion engine
mini UAVs—could serve such a purpose.
produces a higher thrust-to-weight ratio than does the electric
This paper provides a basic understanding of the
motor, the benefits of electric motors are significant. Some experi-
aerodynamic scaling of mini UAVs and a sense of how their
mentation in this regard has begun through programs such as the
capabilities could be matched with specific missions. Mini UAVs 2Marine Corps Dragon Eye program.
have substantial limitations, but the low radar cross section,
low infrared signature, low acoustic signature, and birdlike
Aerodynamic Characteristics
appearance of these vehicles, combined with the remarkable
To address the aerodynamic regime of interest, this papercapabilities of miniaturized payloads, make them contenders
examines five UAVs. The first three vehicles (Extender, Dragon Eye,for certain missions and potential valuable tactical assets.
and MITE) were developed by the air vehicles group at the Naval
3Research Laboratory. The fourth vehicle was developed by the microA New Class of Aircraft
4air vehicle design team at the University of Notre Dame. The fifth
A class of low-altitude unmanned aerial vehicles (UAVs) is 5vehicle, Black Widow, was developed by AeroVironment, Inc. The
currently under development. Several desirable features in their
physical characteristics of theses vehicles are summarized in table 1.
composition warrant discussion. This class of fixed wing vehicles is
All are electrically powered except for the Notre Dame one, which is
larger than the micro UAVs that have received publicity in the past
included because detailed lift and drag data were available providing
1several years, but substantially smaller than the Predator class
UAV. This paper considers vehicles, henceforth called mini UAVs,
that have wingspans ranging between 6 inches and 10 feet and that Table 1. General Characteristics of UAVs
fly in the 20- to 50-mile-per-hour (mph) range (the aerodynamic
Maximum regime typical of model airplanes and birds). While this regime is
Unmanned Wing Span Aspect Weight of Gross
not glamorous, significant developments have occurred in recent Aerial Vehicle (inches) Ratio Structure Weight
years. The new class of aircraft is more capable and rugged than Extender 122 11.35 5.76 lbs. 31.5 lbs.
typical model airplanes but less capable than birds, especially in Dragon Eye 45 3.75 1.5 lbs. 4.5 lbs.
terms of control systems. These developments, plus the arrival of a
MITE 18.5 1.85 4 oz. 10 oz.
variety of low-cost but capable payload technologies, make this a
Notre Dame vehicle 10 1 0.53 oz. 3.7 oz.subject worthy of consideration.
Black Widow 6 1 0.34 oz. 2 oz.
December 2002 Defense Horizons 1Figure 1. Weight Budgets for 20-Minute Flight
Dragon EyeExtender MITE Black Widow
OtherOtherOther
Other 9% 6%9%Structure13% Payload
18% Structure12%
Payload 17%Structure
Structure18%Payload 30%
Propulsion 38%26%
and Power
13%
PropulsionPropulsionPayload Propulsion and Powerand Power56% and Power 62%38%
35%
scaling to aspect ratio one. These data were not available for the maximum weight available for payload (W ) is achieved when bat-m
aspect-ratio-one Black Widow vehicle. tery weight is reduced to zero and the maximum powered flight time
For the purposes of this paper, we assume that the three design is achieved when payload weight (W ) is zero, with the payload beingp
teams that developed the vehicles in table 1 have produced an opti- replaced totally by batteries. Assuming a linear variation between
mized design for each aircraft. Our intention is to investigate the scal- these two limits and using the data provided by the Naval Research
ing of these aircraft as we vary the aircraft size and aspect ratio and Laboratory (NRL), we constructed figure 2, which estimates pow-
determine how this relates to the payloads that this class of UAVs can ered mission duration versus payload weight for each NRL vehicle.
carry for a specific mission and duration. As can be seen from table 1, Data was not available for Black Widow, but it is expected to follow
the vehicles cover an order of magnitude range in wingspan and in a curve similar to MITE. The Notre Dame vehicle was not electrically
aspect ratio and cover two orders of magnitude in vehicle weight. An powered and therefore is not included in figure 2. Figure 2 is used in
immediate practical conclusion can be drawn from table 1 relating to the following sections to examine various payloads that might fly on
the ability of these vehicles to fly autonomously. A competent, com- these or similar vehicles.
mercially available autopilot for low-flying vehicles will weigh from 4 The term powered flight is used deliberately above. It will
6to 6 ounces. MITE and smaller size vehicles with their low weight become clear in the following sections, as it does from figure 1, that
restrictions will be hard pressed to undertake autonomous flight with powered flight duration will be very limited for the small, aspect-
present technology. Dragon Eye-class and larger mini UAVs have ratio-one vehicles. Increasing the reach of these mini UAVs will be
ample capacity to carry an autopilot, and we assume that they do in necessary, and there are very desirable techniques to accomplish
the remainder of this article. this. For example, these vehicles can undertake unpowered flight by
Payload carrying capacity is key to assessing the mission capa- gliding, providing an opportunity to increase range. From a 5-mile
bilities of these vehicles. Figure 1 provides an estimate of the weight release altitude, the Extender has the capability for a 77-mile glide;
budgets for each electrically powered vehicle when sufficient battery the Dragon Eye, 37 miles; MITE, 34 miles; and Black Widow, 25
power is provided for a 20-minute flight. Twenty minutes is selected miles. Of course, technical issues connected with the release of the
because it begins to tax the smaller vehicles’ ability to carry any sort mini UAVs would need to be addressed.
of meaningful payload. Even for such short flight times, it is clear These glide distances assume zero windspeed. Depending on
from figure 1 that power and propulsion begin to dominate the windspeed and direction, the range could be reduced or extended.
weight