Richardson, Robert Charlwood, III, Brig Gen

Deceased
 
 Service Photo   Service Details
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Last Rank
Brigadier General
Last Primary AFSC/MOS
00066-Air Commander
Last AFSC Group
Command and Control
Primary Unit
1966-1967, Defense Atomic Support Agency (DASA)
Service Years
1939 - 1967
Officer srcset=
Brigadier General

 Last Photo   Personal Details 

34 kb


Home State
Illinois
Illinois
Year of Birth
1918
 
This Military Service Page was created/owned by AB Raymond Guinn to remember Richardson, Robert Charlwood, III, Brig Gen USAF(Ret).

If you knew or served with this Airman and have additional information or photos to support this Page, please leave a message for the Page Administrator(s) HERE.
 
Contact Info
Home Town
Rockford
Last Address
Alexandria, VA
Date of Passing
Jan 02, 2011
 
Location of Interment
U.S. Military Academy West Point Post Cemetery (VLM) - West Point, New York
Wall/Plot Coordinates
Section II, Row A, Site 15

 Official Badges 

Headquarters Air Force Commander Air Force Retired Headquarters Command, USAF

Joint Chiefs of Staff US European Command Supreme Headquarters Allied Forces Europe (SHAPE)


 Unofficial Badges 

Cold War Medal


 Military Associations and Other Affiliations
National Cemetery Administration (NCA)
  2011, National Cemetery Administration (NCA)


 2003-2003, P-61 Black Widow
From Year
2003
To Year
2003
   
Personal Memories
Not Specified
   
Image
 P-61 Black Widow Details
 


Aircraft/Missile Information
General characteristics

* Crew: 2-3 (pilot, radar operator, optional gunner)
* Length: 49 ft 7 in (15.11 m)
* Wingspan: 66 ft 0 in (20.12 m)
* Height: 14 ft 8 in (4.47 m)
* Wing area: 662.36 ft² (61.53 m²)
* Empty weight: 23,450 lb (10,637 kg)
* Loaded weight: 29,700 lb (13,471 kg)
* Max takeoff weight: 36,200 lb (16,420 kg)
* Powerplant: 2× Pratt & Whitney R-2800-65W Double Wasp radial engines, 2,250 hp (1,680 kW) each
* Propellers: four-bladed Curtiss Electric propeller, 1 per engine
o Propeller diameter: 146 in (3.72 m)
*

* Main wheel track: 17 ft 2 in (5.24 m)
* Fuel capacity:
o Internal: 640 US gal (2,423 L) of AN-F-48 100/130-octane rating gasoline
o External: Up to four 165 US gal (625 L) or 310 US gal (1,173 L) tanks under the wings
* Oil capacity: 22 US gal (83.3 L) of AN-0-8 oil per engine

Performance

* Maximum speed: 318 knots (366 mph, 589 km/h) at 20,000 ft (6,095 m)
* Combat range: 530 nm (610 mi, 982 km)
* Ferry range: 1,650 nm (1,900 mi, 3,060 km) with four external fuel tanks
* Service ceiling 33,100 ft (10,600 m)
* Rate of climb: 2,540 ft/min (12.9 m/s)
* Wing loading: 45 lb/ft² (219 kg/m²)
* Power/mass: 0.15 hp/lb (25 W/kg)
* Time to altitude: 12 min to 20,000 ft (6,100 m) (1,667fpm)

Armament

* Guns:
o 4× 20 mm Hispano M2 cannon in ventral fuselage, 200 rounds per gun
o 4× 0.50 cal (12.7 mm) Browning M2 machine guns in upper turret, 560 rounds per gun
* Bombs: for ground attack, four bombs of up to 1,600 lb (726 kg) each or six 5 inch (127 mm) HVAR unguided rockets could be carried under the wings. Some aircraft could also carry one 1,000 lb (454 kg) bomb under the fuselage.

Avionics

* SCR-720 (AI Mk.X) search radar
* SCR-695 tail warning radar




   
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Last Updated: Sep 8, 2012
   
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