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From
December '96 Bronco Flyer
A
Plane With a Purpose
Designed With a Purpose
Once Upon a Time
Baby Bronco Plans Available
A
Plane With a Purpose
A quick
look at the OV-10 reveals it to be an unconventional airplane Its wide-spread
twin booms and forward thrusting crew and cargo pod suspended from a broad
rectangular wing, high-mounted, squared-off horizontal stabilizer, negative
dihedral stub sponsons and wide-stance, trailing arm landing gear are
distinctive features that indicate a functional design approach to fulfilling
a variety of mission requirements.
TANDEM
CREW STATIONS
Tandem crew stations positioned well ahead of the wing and engines provide
unobstructed panoramic visibility on both sides of the airplane. The extra
large canopy has minimum support structure and arches overhead and to
the rear of the observer, allowing uninterrupted ground scanning. Over-the-side
vision is 86 degrees from the pilot's cockpit and 75 degrees from the
observer's cockpit, with approximately 90 percent overlap between both
crewmen. With slight head movement, the pilot has 45 degrees visibility
over the nose. A 30 degree bank permits total visibility beneath the airplane.
This unexcelled visibility allows close-in search down to treetop level
and effective operations under low ceilings
LANDING
GEAR
The OV-10 has a demonstrated capability for absorbing the high impact
loads associated with operations from very rough and soft fields at high
sink rates (18.8 feet per second). The wide-stance landing gear's trailing
arm design with large low-pressure tires minimizes footprint pressures
(CBR-4) to assure a capability for extended operation from unimproved
runways in forward areas. The landing gear has been demonstrated at speeds
up to 95 knots on a specially constructed field so rough that automobiles
cannot exceed 13 mph without loss of control.
SPONSONS
The sponsons provide four 600-pound capacity store stations as well as
the internal mounting of guns close to the airplane's centerline and center
of gravity. Alongside the 1200-pound capacity centerline store station,
this cluster arrangement permits a diverse and asymmetrical loading with
minimal effect on airplane aiming and handling characteristics. In addition.
ordnance loading is facilitated by the sponsons' ideal height above ground
level. Although weight and drag of the sponsons is not significant to
airplane performance, they may be easily removed if desired.
TWIN
BOOMS
The twin boom design creates a dedicated crew/cargo pod uncluttered with
engine accommodations. It provides widely separated engine and control
housings which enable isolation of battle damage. In addition, the twin
booms permit the mounting and enclosure of wide-span, large-wheel landing
gear.
CARGO
BAY
The space and strength provisions of the dedicated cargo bay plus available
power and plumbing make possible the accommodation of a number of special
equipment installations. The cargo area is 75 cubic feet with the rear
cockpit seat in, or 110 cubic feet with the seat out. The high booms,
horizontal stabilizer and rear cargo bay door (which opens 180 degrees
and can be removed) permit waist-level loading and unobstructed bail-outs
or supply drops.
Designed
With a Purpose
STOL PERFORMANCE
The propeller slipstream over the broad wing from two turboprop engines
coupled with double slotted trailing-edge flaps comprise the high-lift
system which makes the OV-10 a STOL airplane. The airplane is operational
from strips no longer than 1200 feet depending on altitudes and temperatures.
This STOL capability combined with rough field gear and low support requirements
ensures that the OV-
MAINTENANCE
The design of the OV-10 was based on the criteria of system simplicity
and ease of maintenance. Operational, proven system components are used
throughout. Only standard hand tools are required for forward area maintenance
and no spe- cial ground support equipment is necessary. The T-76 engines
can operate on a variety of fuels. In addition to JP fuels and aviation
gasoline, the engine will also operate on automotive gasoline usually
available in forward areas.
MANEUVERABILITY
A wide speed range, moderate wing loading (35 to 40 pounds) and high struc-
tural strength (sustained normal loads between +6.5 and -1.0 "g's")
plus quick and positive control response permit extremely tight turns
and maneuvers for a variety of tactics and evasive actions. Low, slow,
close-in search is possible even in rugged terrain. At the other extreme,
high speed dives (350 knots) and associ- ated rapid zoom recoveries are
available. In addition, the sturdy, broad wing provides adequate space
for the entire internal fuel supply.
Once
Upon a Time
Well before
the OV-10A was fully operational, North American Aircraft designers at
the Columbus. Ohio division were hard at work looking at derivatives of
the original design.
This transport
concept from a 1966 brochure bears a stnking resemblance to the Special
Operations Transport built about 25 years later by the Rutan operation
in Mojave California.
The proposed
OV-10 transport version was designed to be capable of carrying 14 troops
or 6,000 pounds of cargo. Usable deck area was 73 square feet. For medical
evacuation, six litter patients and six walking wounded could be carried.
Alternate use as a VIP mission support provided seating for eight passengers.
Straight-in loading was accomplished through a large, 60-inch wide door
ramp at the rear of the fuselage. There was a high degree of systems,
logistics and training commonality between the basic OV-10 and the transport
airplane.
TRANSPORT VERSION
Passenger or Cargo Space:
4 feet 8 inches width
5 feet 11 inches height
14 feet 2 inches length
73 square feet deck area
Baby
Bronco Plans Available
On November
14 1996 PALMER PLANS announced final drawing release for the Radio Control
Ov-IOA "Bronco" with a 96" wing span. Because of the drawings
and original engineering data that are in Maney Aircraft's possession
and which were provided to Palmer Plans, the model is an authenitic reproduction
of the full-size aircraft.
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Vital
Statistics for the RC Model Include:
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Wing
span:
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96
in.
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Overall
length:
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99.8
in.
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Wing
area:
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1670.4
sq. in.
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Target
weight:
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15
lb. 6.24 oz. excluding fuel
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Wing
loading:
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22.036
oz. per sq. ft.
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RC
operation:
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7
channels incl. flaps & retracts
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Engines:
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2
each, Saito FA-80's with mufflers
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The plans
consist of four 36' x 72' sheets plus a detailed step by step instruction
manual. They are now available by mail order, shipped rolled up via UPS,
at a price of $74.00 which includes shipping and handling. Visa or Mastercard
are accepted.
PALMER PLANS
has gained reputation among RC model enthusiasts for authen- tic designs
of significant historic aircraft. They conduct extensive research into
original manufacturer's production draw- ings and take careful measurements
of available examples of the "breed".
To order
your plans, contact:
PALMER PLANS, DEPT. MA
6047 Pomegranate Lane
Woodland Hills CA 91376
Phone: 818-348-0879
Fax: 818-348-9204
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