Tizard Mission introduces Airborne Radar to the U.S.

The Tizard Mission, officially the British Technical and Scientific Mission, was sent to the United States in the autumn of 1940 for the purpose of providing the US military services with information on the various technical advances being made by Great Britain during the war against Germany. Members of the mission planned to brief the armed services on British advances being made in jet engines, rockets, and, most importantly, radar. The mission was headed by Sir Henry Tizard, chairman of the Great Britain's Aeronautical Research Committee and included Dr. E. G. "Taffy" Bowen, Britain's leading expert on airborne radar.

Tizard Mission brought two pieces of radar technology that were crucial in jump-starting the United States efforts in the future development of airborne radar. The first of these was the cavity magnetron. This highly secret device solved the problem of generating high power microwaves. Its disclosure to the academic community in the United States quickly led to the establishment of the government sponsored Radiation Laboratory at MIT. The laboratory's personnel were immediately directed to begin development of three important microwave systems: a 10 cm airborne interception radar, a 10 cm gun-laying director, and an electronic navigation system (LORAN). The second were examples of latest airborne radars in use by the Royal Navy and the RAF. In November 1040, a Mk IV radar was fitted to a Douglas A-20 at Wright Field and demonstrated to the Army Air Corps, which was so impressed with the system that plans to manufacture an equivalent radar set in the United States were immediately implemented.



USAAF P-70 night fighter

SCR-540 1.5m Radar

American Version of British Mk IV Radar. Manufactured by Western Electric, delivered 1942 for installation in USAAF P-70 (right) and Marine Corps PV-1 (lower right) night fighters. First confirmed combat kill April 19, 1943, 6th NFS, Guadalcanal.

Description
1.55 cm airborne radar for aircraft interception. Weight: 181 lb including cables and inverter. Operators: 1. Power: 40 amp, 27 volt DC. Antenna: fixed quarter wave dipole with directors on side of fuselage (azimuth receiving): 2 fixed quarter wave rods, one above and one below wing (elevation receiving). Indicators: 3-inch CRT with vertical baseline target pips on left and right (azimuth): 3-inch CRT with horizontal baseline, target pips above and below (elevation).


USMC PV-1 night fighter of VMF(N)-531 at Vella La Vella, Solomono Is, 13 Jan 1944Research and Development By
British and Bell Telephone Laboratories

Performance
Max. Range on:Bombers, at 20,000 ft:6000 yd.
Fighters at 17,000 ft:4000 yd.
Minimum range:300 to 500 ft
Range Accuracy:300 yds.
Angular Accuracy:10° Elevation 10°

Search
Fixed antenna, targets within forward hemisphere 160° elevation sector may be detected. Effective search range limited to altitude of plane.

Antenna Specifications

Transmitting: Bent folded dipole with director on nose of aircraft. Elevation receiving: 2 fixed quarter wave rods with directors, one above and one below the left wing. Lobe switching at 1750 cycles per minute.

SCR-540 elevation antenna, transmitting antenna, and azimuth receibing antennae  on wing of A-20

Anntenna installation on A-20 (prototype P-70), left-to-right: elevation receiving antenna, transmitting antenna, azimuth receiving antenna.

Transmitter Specifications

Frequency:193 mc/sPusle Rate (pps):750 to 850
RF Source:2 710s push-pullPulse Rate Beacon:750 to 850 nps
RF Lines: Coax (solid dielectric)Pulse Legnth:1.3 µs
Pulser Type:Hard TubePulse Length, Beacon:2.1 µs
RF Peak Power: 10 kwEnergy pp, Radar:.013 joules
RF Average Power: .01 kw


Receiver Specifications

Type:SuperheterodyneIF Band Pase:5 mc/s
Stages:O-RF; 4-IFMixer:955 tube
Local Oscillator: 955Noise, db above kt df:14-16
Intermed. Freq.:30 mc/s


Indication and Data Output
Operator has indicator with two 3-inch CRTs. Left tube has horizontal sweep with echoes appearing as pips above and below searching plane. Right tube operates similarly but has a vertical sweep with left and right pips indicating whether target is to the left or right of searching plane. Time scales are variable and the distance for a given length of trace depends on control setting. Scale is exponential. Attack range: 1-7 miles. Homing range: 100 miles.


Remarks
Maximum altitutde for satisfactory operation: Approximately 20,000 ft. Operates with SCR-640 homing beacon.
Generally not employed to control an area when prsence of enemy aircrft has not been determined in advance. SCR-540-T2 is similar to SCR-540-A except for minor circuit differences.


SCR-520 system components
click image to enlarge

SCR-520 10 cm Radar

First 10 cm Radar developed for installation on P-70. Most SCR-520s were converted to SCR-517 for ASV.

Wavelength and Function
10 cm airborne radar for aircraft interception.

Research and Development By
Radiation Laboratory and Bell Telephone Laboratories

Operational Requirements

Number of Operators:1Weight:477 lb. less cables

Power Supply:125 amp, 27 v DC;
 inverter delivers 1520 w, 115 v. 1 ph, 400 cps

Performance
Max. Reliable Range on:Bombers, at 10,000 ft:10,000 yd.
Fighters at 17,000 ft:6,000 yd.
Minimum range:125 yd.
Range Accuracy:±10° full scale
Angular Accuracy:Azimuth ±3° Elevation ±3

Search
Antenna spins at 360 rpm and searches the forward 180° sector. While spinning, antenna tilts at rate of 30°/sec. between limit which can be set at -10° to 45°, +20°, +35°, +50°,or +65°. Range: 1, 10, and 100 miles. Beacon operation on 10-.

Antenna specifications
Vertically polarized dipole in 30-inch paraboloid. Antenna sons at 360 rpm. As it rotates, the antenna tilts up and down at the rate of 30° per second.
Half power basewidth: 10° azimuth and elevation.
Gain: 340.

Transmitter Specifications

Frequency:3000 mc/sPusle Rate(pps):2000
RF Source:MagnetronPulse Rate Beacon:400 pps
RF Lines: 7/8 inch stub Coax Pulse Legnth:1.3 µs
Pulser Type:Hard TubePulse Length, Beacon:2.5 µs
RF Peak Power: 40-60 kwEnergy pp, Radar:0.05 joules
RF Average Power: .01 kw

Receiver Specifications
Type:SuperheterodyneIF Band Pase:4 mc/s
Stages:O-RF; 7-IFMixer:708A tube
Local Oscillator: 707ANoise, db above kt df:19-21
Intermed. Freq.:60 mc/s

Indication and Data Output
Operator: 1 5-inch CRT with type-B scan and 1 5-inch CRT with type-C scan. Inaddition to range switch, systm has range dial and targets seen on C-Tube lie between setting of tis dial and pooints 0.5 miles near plane bearing equipment. Pilot: 1 5-inch CRT with type-C scan displaying only the targets seenon the operator's C-Tube. Pilot obtains range from a range meter.

Remarks
Equipment will operate under temperatures from -40°F to +122°F, with relative humidity as high as 90%. Max.altitude for satisfactory operation: 30,000 ft. SCR-520-B differs from SCR-520-A by the addition of beacon and IFF features and a 100 mile range.

Procurement and Production
Manufacturer:Western Electric
Number ordered:108
Procuring ServiceU.S. Army
Number delivered:108
Unit Cost:$17,765
Value of delivered units:$1,918,620


USAAF P-61 in flight

SCR-720 10 cm Radar

Improved SCR-520 developed for installation on P-61 (right), P-70 and DeHaviland Mosquito.

Wavelength and Function
10 cm radar for air search with beacon functioins and connections to IFF. Similar in purpose to SCR-520-A and B, but components are smaller and lighter in weight. Manufactured by Western Electric.

Research and Development By
Bell Telephone Laboratories

 

 

P-61  radar equip. layout
click image to enlarge
Operational Requirements
Number of Operators:1Weight:415 lb. less cables

Power Supply:125 amp, 27 v DC;
 inverter delivers 1520 w, 115 v. 1 ph, 400 cps

 

Performance
Max. Reliable Range on:Bombers, at 10,000 ft:17,000 yd.
Fighters at 17,000 ft:8,500 yd.
Minimum range:100 yd.
Range Accuracy:±10° full scale
Angular Accuracy:Azimuth ±3° Elevation ±3°

Search
Ranges: 1, 10, 20, and 100 statute miles. Azimuth Search: 180° forward sector. Elevation Search: operator may select any one of 4 sectors: 0° to 0° (level), -5° to +5°, +5° to +20° and +20° to +50°. In later models the ranges are changed to 5 miles, expanded sweep (dog leg), 10 20, and 100 statute miles.

Exposed nose of P-61 showing scanning antennaAntenna specifications
Dipole antenna with 29-inch paraboloid reflector (right) spinning at 360 rpm (2, 10, or 20 mi. radar) or 100 rpm (100 mi. radar or 10, 20, or 100 mi. beacon).
Half power basewidth: 10° azimuth and elevation.
Gain: 340.

Transmitter Specifications

Frequency:3000 mc/sPusle Rate(pps):1500
RF Source:MagnetronPulse Rate Beacon:375 pps
RF Lines: 7/8 inch stub Coax Pulse Legnth:0.75 µs
Pulser Type:Rotary gapPulse Length, Beacon:2.5 µs
RF Peak Power: 100-150 kwEnergy pp, Radar:0.08-.11 joules
RF Average Power: .0.112-.17 kw

Receiver Specifications
Type:SuperheterodyneIF Band Pase:3 mc/s
Stages:O-RF; 6-IFMixer:Crystal (IN21)
Local Oscillator: 726ANoise, db above kt df:11-15
Intermed. Freq.:60 mc/s

P-61 cockpit details

Indication and Data Output
Operator Station (far right): 1 5-inch CRT with type-B scan and 1 5-inch CRT with type-C scan.
Pilot's CRT (near right): 1 -3-inch type B (20 and 100 mile search and 10, 20, and 100 mile beacon), or type C (2 and 10 mile search). Vertical scale on C-tube extends from -15&deg to +60&deg. C-tube shows only targets within limits of range dial setting. Pilot also has range meter.

Remarks
Equipment will operate under temperatures from -40°F to +122°F, with relative humidity as high as 90%.
Max.altitude for satisfactory operation: 30,000 ft.
SCR-520-B differs from SCR-520-A by the addition of beacon and IFF features and a 100 mile range.


F4U-2N preparing for takeoff

AIA 3 cm Radar

Air Interception Radar For Carrier Based Fighters for installation on F4U-2N (top right) and F6F-3N (bottom right) night fighters.

Wavelength and Function
3.2 cm radar for surface search and air interception. Provides beacon function and has connections for IFF.

Research and Development By
Radiation Laboratory and Sperry Gyroscope Co., Inc.

Operational Requirements

Number of Operators:1Weight:242 lb. less cables

click image to enlarge
Power Supply:25 amp, 27 v DC, and
 700 w, 115 v. 1 ph, 400 to 2400 cps

Performance
Max. Reliable Range on:Bombers, at 10,000 ft:8,000 yd.
Fighters:7,500 yd.
 Battleships30 miles
Minimum range:150 yd.
Range Accuracy:±10° full scale
Angular Accuracy:Azimuth ±3° Elevation ±20°
Search range scale to 4 miles
Conical scan accurate aiming to 1000 yd.

Search
Spiral scan through 120° cone ( ±60° from plane axis) at 15 scans per minute for 4 mile search and 100 mile operations. Conical with 10° covered operation on "Sight."

Target Following
Aiming by pointing plane in conjunction with conical scan and aiming error indicator (Type G).

Antenna specifications
Rotating and nodding 17-inch paraboloid with waveguide feed.
Half power beam width: 4.5° in azimuth and elevation.
Gain: 1500.

Transmitter Specifications

Frequency:9375 mc/sPusle Rate(pps):2000
RF Source:MagnetronPulse Rate Beacon:500 pps
RF Lines: 1 inch x 1 1/8 inch waveguidePulse Legnth:0.5µs
Pulser Type:Hard TubePulse Length, Beacon:2.1µs
RF Peak Power: 40 kwEnergy pp, Radar:0.02 joules
RF Average Power: .01 kw

Receiver Specifications
Type:SuperheterodyneIF Band Pase:2.6 - 4 mc/s
Stages:O-RF; 7-IFMixer:IN23A crystal
Local Oscillator: 723A/BNoise, db above kt df:16
Intermed. Freq.:30 mc/s

Indication and Data Output

3-inch indicator with type G scan with 0.5 nautical mile range for "Sight", type O (double dot) scan with 4 nautical mile range for "Search", and B scan for 100 nautical mile search and beacon range.

Procurement and Production
Manufacturer:Sperry Gyroscope Company
Number ordered:750 (146 cancelled)
Procuring ServiceU.S. Navy
Number delivered:604
Unit Cost:$8,618
Value of delivered units:$5,205,272


F6F-3N preparing for takeoff

AN/APS-6 3 cm Radar

Lightweight Search and Intercept Radar. For installation in F6F (right) and F7F fighters.

Wavelength and Function
3 cm search and interception radar for carrier based aircraft. Provides beacon function and has connections for IFF, and provides suitable indication for firing guns. Major improvement over AIA was placement of modulator in nacelle close to scanner, which elimnated long wave guide runs that were difficult to install and maintain.

Research and Development By
Radiation Laboratory and Westinghouse Electric and Mfg. Co., Inc.

Operational Requirements

Number of Operators:1Weight:242 lb. less cables

Power Supply:29 amp, 27 v DC, and
 780 w, 115 v. 1 ph, 800 to 2400 cps

Performance
Max. Reliable Range on:Bombers, at 10,000 yd.10,000 yd.
Fighters, 8,000 yd.8,000 yd.
 Battleships35 miles
Minimum range:120 yd.
Range Accuracy (search mode)±10° +2° full scale
Range Accuracy (aiming)25 yd. at firing point of 250 yd.
Angular Accuracy (search, mode)±3° Azimuth and Elevation
Angular Accuracy (aiming)±0.5° Azimuth and Elevation
Search range scale to 4 miles
Conical scan accurate aiming to 1000 yd.

APS-6 Field of view

Search
Spiral scan through ±60° at 1200 rpm (120° cone along forward axis of aircraft). Search ranges of 1, 5, 25, and 65 nautical miles. 1000 yd range for close approach and gun aiming. Beacon ranges: 1, 5, 25, and 100 nautical miles.

Target Following
Fixed guns are aimed by pointing plane.

Antenna specifications
Dipole in rotating and nodding 17-inch paraboloid.
Half power beam width: 5° in azimuth and elevation.
Gain: 1100.

Transmitter Specifications

Frequency:10,000 mc/sPusle Rate(pps):2000
RF Source:MagnetronPulse Rate Beacon:500 pps
RF Lines: waveguidePulse Legnth:0.5µs
Pulser Type:Hard TubePulse Length, Beacon:2.0µs
RF Peak Power: 40 kwEnergy pp, Radar:0.02 joules
RF Average Power: .04 kw

Receiver Specifications
Type:SuperheterodyneIF Band Pase:2.7 mc/s
Stages:O-RF; 7-IFMixer:IN23 crystal
Local Oscillator: 723A/BNoise, db above kt df:16
Intermed. Freq.:60 mc/sAFC optional
Separate Oscillator for BeaconAVC aiming only

Indication and Data Output
3-inch indicator CRT: B scan on search and beacon ranges with type O scan on 1 and 5 mile search range. Type G scan for aiming.

Remarks
AN/APS- 6 uses Westinghouse RF head with radar and beacon AFC. AN/APS-6A uses Philco RF head and has no beacon AFC.

Procurement and Production
Manufacturer:Westinghouse Electric
Number ordered:3129
Procuring ServiceU.S. Navy
Number delivered:2161 as of 8/1/45
Unit Cost:$10,938
Value of delivered units:$23,632,696

AN/APS- 6 Pilot's Manual
First Page of Pilot's Manual

Sources

Guerlac, Henry E., Radar in World War II. American Institute of Physics, 1987.

National Defense Research Committee Divison 14, Final Project Report. Cambridge, MA: Office of the Secretary, Divison 14 of the National Defense Research Council, 1945.

U.S. Radar Survey: Section 1 Airborne Radar. Washington, DC: National Defense Research Committee, 1944.

Westinghouse Electric & Mfg. Co., Inc. "The AN/APS-6 Aircraft Radar," in Westinghouse in World War 2: Radio and X-ray Divsions, Book 1, Westinghouse Electric & Mfg.Co., Inc, 1946.

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