

Like the RF-4C, the RF-4B was unarmed. The
fighter's radar-equipped nose was replaced
with a special nose specifically designed
for reconnaissance applications. This nose
(Fig.01) was 4 feet 8 7/8 inches longer than
the nose of the armed F-4B. The AN/APQ-72
radar of the F-4B was replaced by the much
smaller Texas Instruments AN/APQ-99 (Fig.02)
forward-looking J-band monopulse radar which
was optimized for terrain avoidance and terrain-following
modes, and could also be used for ground
mapping. The rear cockpit (Fig.03) was configured
for a reconnaissance systems operator, with
no flight controls being provided. Two ALE-29A/B
chaff/flare dispensers (Fig.04) were installed,
one on each side of the aircraft above the
rear fuselage. For nighttime photography,
a set of photoflash cartridges could be ejected
upward from each side of the aircraft. An
AN/APQ-102 reconnaissance SLAR was fitted,
with antenna faired into the lower fuselage
sides (Fig.05) , just ahead of the intakes.
This SLAR was capable of tracking both fixed
and moving targets. An AN/AAD-4 infrared
reconnaissance system was fitted in the fuselage
belly just behind the SLAR. AN APR-25/27
radar homing and warning system was used,
an ASW-25B one-way datalink was installed.
An ALQ-126 deceptive electronic countermeasures
package was installed, which obviated the
need to carry external jammer pods. An ARC-105
communication transceiver was fitted, which
required that large fin-skin shunt antennae
be faired into both sides of the vertical
fin. A Litton ASN-48 inertial navigation
system was carried.
The first 34 RF-4Bs (BuNos 151975/151982 and
152089/153113) retained the powerplants and
the basic airframe of the F-4B. However,
the last twelve (BuNos 153114, 153115, and
157342/157351) were built with the wide wheels
(Fig.06) and the "thick" wing (Fig.07)
of the F-4J. The last three of these (157349/157351)
were completed with the smoothly-rounded
undernose bulge (Fig.08) similar to that
seen on many USAF RF-4Cs. This adaptation
improved the aerodynamics and increased the
internal volume. However, on these three
aircraft, the pilot no longer had control
of the angle of a KS-87 camera on station
2, which was made fixed. The film could be
developed in flight and film cassettes could
be ejected at low altitude so that ground
commanders could get aerial intelligence
as rapidly as possible.
There were three separate camera bays in the
nose, designated Stations 1, 2, and 3. Station
1 could carry a single forward oblique or
vertical KS-87 camera, Station 2 could carry
a single KA-87 low-altitude camera, and Station
3 normally carried a single KA-55A or KA-91
high-altitude panoramic camera. The much
larger KS-91 or KS-127A camera could also
be carried. Unlike the cameras of the Air
Force's RF-4Cs, the RF-4B's cameras were
fitted on rotating mounts so that the pilot
could aim them at targets off the flight
path.
Trivial Information
During the Southeast Asia conflict, three
RF-4Bs were lost to ground fire and one was
destroyed in an operational accident.Beginning
in 1975, surviving Marine Corps RF-4Bs were
upgraded as part of Project SURE (Sensor
Update and Refurbishment Effort). There was
some local strengthening of the airframe
and the wiring was entirely replaced. These
planes were fitted with the AN/ASN-92 carrier
aircraft inertial navigation system (CAINS)
which replaced the ASN-48. They were also
fitted with the AN/ASW-25B datalink, the
AN/APD-10B SLAR (replacing theAPQ-102A),
and the AN/AAD-5 infrared reconnaissance
set (replacing the AN/AAD-4). Various externally-mounted
electronic countermeasures pods were replaced
by the internally-mounted ALQ-126 or -126B
electronic countermeasures suite with characteristic
cable ducts mounted on the sides of the intakes.
The J79-GE-8 engines were later replaced
by J79-GE-10 engines. In 1975, two years
after combat in Southeast Asia had ended,
the surviving RF-4Bs were regrouped into
a new squadron, VMFP-3, based at MCAS El
Toro. VMFP-3 stood down in August of 1990,
bringing Marine Corps operations of the RF-4B
to an end.

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