SNORA and SURA-D rockets

SNORA
Type	Unguided air-to-surface and surface-to-surface rocket
Place of origin	Switzerland
Service history
In service	1980's
Used by	Swiss Air Force
Production history
Manufacturer	Oerlikon-Bührle
Variants	High-explosive fragmentation and hollow-charge
Specifications
Weight	See table
Length	Varies by model
Caliber	81-mm warhead
Muzzle velocity	See table
Maximum range	10 kilometers

SURA-D
Type	Unguided air-to-surface rocket
Place of origin	Switzerland
Service history
In service	1980's - present
Used by	Swiss Air Force
Production history
Manufacturer	Oerlikon-Bührle
Variants	High-explosive fragmentation, hollow-charge, incendiary, marker, and training
Specifications
Weight	See table
Length	Varies by model
Caliber	80-mm warhead
Muzzle velocity	See table
Maximum range	2.5 kilometers

The Oerlikon-Bührle SNORA and SURA-D are 81-mm and 80-mm rockets developed in Switzerland in the late 1970's and fielded in the 1980's. The SNORA could be used in both air-to-surface and surface-to-surface (rocket artillery) roles, while the SURA-D is an air-to-surface rocket. The SNORA was developed as a cooperative endeavor with the Italian firm SNIA-Viscosa (later SNIA-BPD).

History

The original version of the SURA rocket, the SURA 80R, was developed by Hispano-Suiza in the 1960's.^[1] In 1971 Oerlikon-Buhrle took over the military division of Hispano-Suiza and redesignated the SURA 80R, the SURA-FL, and further developed the SURA-FL which is the current SURA-D.^[2] The SNORA rockets can be fired from either a supersonic or subsonic aircraft. The SURA-D though, is limited to subsonic aircraft.

Oerlikon also developed the RWK 014, a surface-to-surface launcher for the type SNORA rockets. The RWK 014 has dual launchers of 15 tubes each and has been mounted on the MOWAG Tornado APC as well as the M113 armored personnel carrier. The RWK 014 can fire 10 rounds per second and has a reload time of six minutes.^[3]

The SNORA rocket was still in service as late as 1998^[4] and the SURA-D is still in operational use. SNORA rockets are launched from a variety of pods housing from either six or twelve rockets,^[5] while SURA-D rockets are mounted as a vertical array with only the top-most rocket attached to an aircraft hardpoint. In this system, rockets are fired individually from the bottom of the tier to the top. The unique sliding fixed fin arrangement of the SURA-D acts as the forward hanger for the rocket below it. As the rocket is fired, the four fixed fins mounted on a ring slide down the body till they are stopped at the expansion area of the rocket motor nozzle and are locked in place. The SURA-D increased its accuracy by the addition of flutes inside the nozzle rear to give a low rotation rate in addition to the stabilization effected by four fixed fins which take effect shortly after launch.

Overview

The 80-mm hollow-charge warhead on the SURA-D has been demonstrated by Oerlikon to penetrate 33 cm (13 in) of armor. The SNORA rocket can mount one of two hollow-charge warheads, either the RAK 026 which can penetrate 35 cm (14 in) of armor, or the RAK 054, capable of penetrating 45 cm (18 in) of armor.^[6][7]

Both rockets were exported by Switzerland and adopted by other nations, among them Spain, Qatar, and Botswana. Italy later used the motor of the SNORA rocket as the basis for the development of the 81-mm Medusa rocket.^[8]

SNORA and SURA-D rocket data

External images
SNORA and SURA-D rockets
	SNORA pod Swiss AF MIRAGE IIIS
	SURA-D rockets Swiss AF Hunter
	SURA-D rocket showing launch example of fins used for mounting
	RWK 014 installed on M113 APC

SNORA rocket type	RAK 023 HE FRAG	RAK 024 HE FRAG	RAK 025 HE FRAG	RAK 026/054 HC	RAK 022 TNG[9]
Warhead weight	4.5 kg (9.9 lb)	7 kg (15 lb)	11 kg (24 lb)	4.5 kg (9.9 lb)	7 kg (15 lb)
Explosive	1 kg (2.2 lb)	1.7 kg (3.7 lb)	2.8 kg (6.2 lb)	1 kg (2.2 lb)	0 kg (0 lb)
Weight of propulsion unit	8.7 kg (19 lb)
Complete rocket	13.2 kg (29 lb)	15.7 kg (35 lb)	19.7 kg (43 lb)	13.2 kg (29 lb)	15.7 kg (35 lb)
Velocity, m/s	820	670	520	820 / 920	670

SURA-D rocket type	RAK 053 HE FRAG	RAK 050 HE FRAG	RAK 052 HE-I	RAK 047 HC	RAK 049 MKR	RAK 051 TNG	RAK 048 TNG
Warhead weight	3 kg (6.6 lb)	4.5 kg (9.9 lb)	3 kg (6.6 lb)	3 kg (6.6 lb)	4.5 kg (9.9 lb)	3 kg (6.6 lb)	4.5 kg (9.9 lb)
Explosive	0.87 kg (1.9 lb)	1.0 kg (2.2 lb)	1.5 kg (3.3 lb)	n/a	n/a	0 kg (0 lb)	0 kg (0 lb)
Weight of propulsion unit	8.4 kg (19 lb)
Complete rocket	11.4 kg (25 lb)	12.9 kg (28 lb)	11.4 kg (25 lb)	11.4 kg (25 lb)	12.9 kg (28 lb)	11.4 kg (25 lb)	12.9 kg (28 lb)
Velocity, m/s	530 - 595

Designation:

• HE FRAG: High Explosive Fragmentation
• HE-I: High Explosive - Incendiary
• HC: Hollow Charge (HEAT)
• MKR: Marker
• TNG: Practice

References

Notes

1. ^ flightglobal.com ad
2. ^ The term "SURA" refers to the method of hanging the rockets in a vertical array on an aircraft.
3. ^ Jane's Infantry Weapons 1984-85, p. 660.
4. ^ Jane's Air-Launched Weapons Issue 35, p. 692.
5. ^ Jane's Weapons Systems 1988-89, p. 750.
6. ^ Jane's Air-Launched Weapons Issue 35, p. 691.
7. ^ The RAK 026 is most likely a dual purpose warhead that has both a light/medium antiarmor ability and a fragmentation ability against personnel and unarmored vehicles.
8. ^ Armada International article
9. ^ There are also RAK 027, 029, 030, and 031 training rockets with overall weights of 19.7, 13.2, 15.7, and 19.7 Kilograms.