This Military Service Page was created/owned by
SSgt Robert Bruce McClelland, Jr.
to remember
White, Robert Michael, Maj Gen USAF(Ret).
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Contact Info
Home Town New York City, NY
Last Address Orlando, Florida
Date of Passing Mar 17, 2010
Location of Interment Arlington National Cemetery (VLM) - Arlington, Virginia
He flew 52 combat missions in WWII, was shot down, and became a POW. He was the first pilot to fly an aircraft at Mach 4, 5, and 6. He flew 70 combat missions in the Vietnam War.
The President of the United States of America, authorized by Title 10, Section 8742, United States Code, takes pleasure in presenting the Air Force Cross to Colonel Robert M. White (AFSN: 0-24589A), United States Air Force, for extraordinary heroism in military operations against an opposing armed force as an F-105 Mission Commander and Pilot of the 355th Tactical Fighter Wing, Takhli royal Thai Air Base, Thailand, in action near Hanoi, North Vietnam, on 11 August 1967. On that date, Colonel White led the entire combat force against a key railroad and highway bridge in the vicinity of Hanoi. In spite of 14 surface-to-air missile launches, MiG interceptor attacks, and intense anti-aircraft artillery fire, he gallantly led the attack. By being the first aircraft to dive through the dark clouds of bursting flak, Colonel White set an example that inspired the remaining attacking force to destroy the bridge without a single aircraft being lost to the hostile gunners. Through his extraordinary heroism, superb airmanship, and aggressiveness in the face of hostile forces, Colonel White reflected the highest credit upon himself and the United States Air Force.
Aircraft/Missile Information
Model Republic F-105D Thunderchief Length 64.24 ft | 19.58 m Width 34.94 ft | 10.65 m Height 19.59 ft | 5.97 m Engine(s) 1 x Pratt & Whitney J75-P-19W turbojet engine generating 24,500lbs of thrust with afterburn capability. Empty Weight 27,500 lbs | 12,474 kg MTOW 52,838 lbs | 23,967 kg Max Speed 1,390 mph | 2,237 km/h | 1,208 kts Max Range 920 miles | 1,480 km Ceiling 41,207 ft | 12,560 m | 7.8 miles Climb Rate 34,400 ft/min (10,485 m/min) Hardpoints 4 Armament 1 x 20mm cannon
Internal bomb load capacity of up to 8,000lbs (3,629 kg) with an overall capacity of 12,000lbs (5,442 kg) of munitions (with the inclusion of the external hardpoints).
Mission-specific armament can include AIM-9 Sidewinder air-to-air missiles, mine dispensers, air-to-surface missiles, rocket pods, fuel tanks, nuclear-tipped weapons and conventional dumb bombs. Accommodations 1
Major Variants
* YF-105A - Initial prototypes of which two produced; Pratt & Whitney J57-P-25 turbojet. * YF-105B - Second prototype of which four produced; J75-P-3 powerplant. * F-105 - Base model designation * F-105B - First production rate model * F-105D - All-Weather Attack Variant * F-105F - Final production designation; Two-seat conversion trainer model. * EF-105F - Wild Weasel conversion with special radar detection equipment and anti-radar air-to-surface missiles. * F-105G - Later designation of same EF-105F Wild Weasel Variant.
