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Arboga Robotmuseum

RB 322

Robothistoriska Föreningen i Arboga

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Sidan uppdaterad: 2017-02-18 14:01

Start

Missile

Engine

Radar

Simulator

 

Missile History

 

V-1 bomb

 

Navy Test missiles

 

Air Force Test missiles

 

Saab Test missiles

 

Air-to-surface missiles

 

Ship-to-ship missiles

 

Coastal missiles

 

Surface-to-air missiles

 

Anti-tank missiles

 

Target missiles

 

Submunition dispenser

 

Missile summary table

 

                                         

Surface-to-air Missile 322

 

The RB 322 was a test missile used in the development of a surface-to-air missile with supersonic speed. The missile is similar to the air-to-air RB 321.It was contemplated as weaponry for the a/c J 35 the Dragon. The American Falcon missiles RB 27 and RB 28 were purchased for this aircraft instead of using the RB 322.

 

http://www.robotmuseum.se/Mappar/Robothistorik/04_Flygvapen/ARM_Rb_322-filer/image004.jpg

 

In essence the RB 321 was attached with a ram jet engine and a booster rocket to achieve the supersonic speed needed for correct efficiency for a ram jet engine (Approx. M = 1.7).

 

The project was never completed but it was used by SvenskaFlygmotor in their development of the ram jet engines.

 

Steering

Themissile was set to a pre-set trajectory by a control unit that included three measuring instruments. Each control unit contained a gyro and a pre-programmed clockwork.

 

Registration

The engine parameters and its vibrations were recorded on a 16-channel tape recorder. The steering values, accelerations and temperature recordings were transmitted to aremote measuring recorder.

The design started in 1951 and the testing was terminated in 1961.

The Chief designer was Chief Engineer Tore Edlén.

 

Data

Length

13 feet 4.5 inches

(4.052 mm)

Diameter

12.6 inches

(320 mm)

Wing span

4 feet 5.5 inches

(1.360 mm)

Missile weight

830 lbs

(377 kg)

Missile weight + booster rocket

2.780 lbs

(1.260 kg med booster)

Boosterrocket

KR 23 C

(Startraket KR 23 C)

Thrust

38.350 lbf

(17.400 kp under 5 sek)

Ram jet engine

RR 2

(Ram motor RR 2)

Thrust

2.200 lbf/engine

(1.000 kp./motor)

Range

50 miles

(80 km)

Speed

M = 2.2 – 2.75

(Hastighet M = 2.2 – 2.75)

(M = 3.1recorded value)

(uppmätt värde M = 3.1)

 

 

 

 

Missile types:

 

RB 301

 

RB 302

 

RB 303

 

RB 304A

 

RB 304B

 

RB 321

 

RB 322