In initial proposals and in pre-contract negotiations, this aircraft
had initially been referred to as F4H-1P. However, this was changed
to RF-4B in September 1962 when the new unified designation scheme
came into effect.
The RF-4B was quite similar to the much more numerous RF-4C of the
USAF. 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 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
forward-looking J-band monopulse radar which was optimized for terrain
avoidance and terrain-following modes, and could also be used for
ground mapping. 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.
The rear cockpit was configured for a reconnaissance systems operator,
with no flight controls being provided. Two ALE-29A/B chaff/flare
dispensers 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, 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 and the "thick" wing of the F-4J. The last three of these
(157349/157351) were completed with the smoothly-rounded undernose
bulge 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.
The first RF-4B flew on March 12, 1965, and deliveries of 46 examples
took place between May 1965 and December 1970. All of them went to
the Marine Corps.
The RF-4B was first delivered to VMCJ-3 based at MCAS El Toro in May
of 1965, and soon after to VMCJ-2 at MCAS Cherry Point and to VMCJ-1
at Iwakuni in Japan.
VMCJ-1 based at Iwakuni in Japan took its RF-4Bs to Da Nang in October
of 1966. 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 the APQ-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.
Serial numbers of the RF-4B:
151975/151977 McDonnell RF-4B-20-MC Phantom (USMC)
151978/151979 McDonnell RF-4B-21-MC Phantom (USMC)
151980/151981 McDonnell RF-4B-22-MC Phantom (USMC)
151982/151983 McDonnell RF-4B-23-MC Phantom (USMC)
153089/153094 McDonnell RF-4B-24-MC Phantom (USMC)
153095/153100 McDonnell RF-4B-25-MC Phantom (USMC)
153101/153107 McDonnell RF-4B-26-MC Phantom (USMC)
153108/153115 McDonnell RF-4B-27-MC Phantom (USMC)
157342/157346 McDonnell RF-4B-41-MC Phantom (USMC)
157347/157351 McDonnell RF-4B-43-MC Phantom (USMC)
Sources:
The World's Fighting Planes, William Green, Doubleday, 1964.
McDonnell F-4 Phantom: Spirit in the Skies. Airtime Publishing, 1992.
The American Fighter, Enzo Angelucci and Peter Bowers, Orion, 1987.
United States Military Aircraft Since 1909, Gordon Swanborough and
Peter M. Bowers, Smithsonian, 1989.
Joe Baugher **************************************
AT&T Bell Laboratories * "Round up the usual suspects." *
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