
SPECIFICATIONS
| WING SPAN |
38’ 5” |
| WING AREA |
530 SQ FT |
| LENGTH |
62’ 11” |
| HEIGHT |
16’ 6” |
| EMPTY WEIGHT |
28,276 LBS |
| GROSS WEIGHT |
54,800 LBS |
| ENGINE |
2 x GENERAL ELECTRIC
J-79-GE-8 |
| THRUST |
10,900 LBS EACH
17,000 LBS
WITH AFTERBURNER |
| MAX SPEED |
1,407 MPH |
| CRUISE SPEED |
580 MPH |
| CEILING |
34,400’ |
| CLIMB |
47,500 FEET PER MINUTE |
| RANGE |
1475 NAUTICAL MILES |
| ARMAMENT |
CAMERAS AND SENSING DEVICES ONLY |
|
|
McDONNELL-DOUGLAS
RF-4B "PHANTOM II"
R - RECONASSAINCE
F - FIGHTER
4 - 4TH MODEL
B - 2ND MODIFICATION
The
Phantom was designed as a fighter, but the Marine Corps
made a recon version. The RF-4B's first flight was 12 March
1965.
All 46 of the RF-4Bs produced went to the Marine Corps.
The last 12 RF-4Bs were built on USAF RF-4C frames with
larger tires, wheel wells and re-enforced wings. The RF-4B
served with Marine Composite Squadrons: VMCJ-1, VMCJ-2
and VMCJ-3. The Navy elected to stay with the RF-8
Crusader and the RA-5 Vigilante, and did not order the
RF-4. This aircraft was accepted 15 October
1965 and delivered to VMCJ-3 at MCAS El Toro, CA and spent
its entire service life with that squadron and its predecessor
Marine Photo Squadron, VMFP-3.
It was retired on 25 April 1990 with 5,364 airframe hours
and presented to the museum. It still wears the colors
of its last unit, VMFP-3. Click here for a larger picture
and more information. |