""BLACK ARROW & KNIGHT""

Black Knight (rocket)

Black Knight

Black Knight BK02
Function	Vehicle for re-entry studies
Manufacturer	Saunders-Roe
Country of origin	United Kingdom
Size
Height	10.2 - 11.6 m
Diameter	0.91 m
Mass	12,500–14,200 lb
Stages	1 - 2
Capacity
Payload to 800 km (Sub-orbital	115 kg
Launch history
Status	Retired
Launch sites	LA-5, Woomera
Total launches	22
Successes	22
Maiden flight	7 September 1958
Last flight	25 November 1965
First stage - Black Knight
Engines	Initially 4 chamber Gamma 201, later 4 chamber Gamma 301 engine.
Thrust	from 15,600 to 21,600 lbf depending on version.
Burn time	120-145 seconds depending on version
Fuel	RP-1/HTP
Second stage (Optional) - Cuckoo
Engines	1 Solid
Thrust	8,200 lbf
Specific impulse	213 seconds
Burn time	10 seconds
Fuel	Solid

Black Knight was a British launch vehicle to test and verify the design of a re-entry vehicle for the Blue Streak missile.
The United Kingdom's first indigenous rocketry project, Black Knight was manufactured by Saunders-Roe on the Isle of Wight, had its engines tested at The Needles and was launched at Woomera in Australia. Designed in 1955 by the Royal Aircraft Establishment and Saunders-Roe, 22 vehicles were fired between 1958 and 1965.

Black Knight tail showing engines

The Gamma rocket engines were designed and built by Armstrong-Siddeley at Anstey, near Coventry. One of the men who designed the engine was C. Donald.
The first two vehicles were 'proving rounds' - that is, launches without a payload in order to prove the design of the rocket. The third firing carried a re-entry vehicle. This flight showed that the chosen design for the re-entry body was a success.
Further firings with different heads showed up some unusual phenomena, and further tests under the code names Gaslight and Dazzle were carried out in conjunction with the United States.
A variety of heads were flown in these tests, including a plain copper sphere and a silica sphere. Heads composed of a composite asbestos-based material known as Durestos were also flown, and later tests finalised on a cone-shaped head re-entering pointed-end first, as used on many subsequent missile RVs.
All the re-entry firings took place on clear moonless nights, so that the luminous wake of the re-entry body could be observed photographically.
An improved Black Knight, with the tank diameter increased from 36 inches to 54 inches, and a more powerful second stage, named Kestrel, was proposed for a further set of experiments codenamed 'Crusade'.
However, the Royal Aircraft Establishment made various studies into extending the vehicle into a satellite launcher. The Treasury refused to fund both projects, and the enlarged Black Knight was cancelled in favour of the Black Arrow satellite launcher.
25 Black Knight vehicles were built in total at a unit cost of just over £40,000 each. One (BK02) was used for ground testing. One (BK11) was fired as part of the ELDO project, to check out range facilities. 21 were fired as part of the re-entry experiments and the remaining two (BK02 and BK22) are in museums in Edinburgh and Liverpool.
The Black Knight BK22 rocket is on display at the Royal Museum Connect Gallery in Edinburgh, Scotland. It stands nearly 11m high and stretches up for three floors.

Black Arrow

From Wikipedia, the free encyclopedia

For other uses, see Black arrow (disambiguation).

Black Arrow

A mockup of the Black Arrow in the rocket park at Woomera.
Function	Carrier rocket
Manufacturer	Royal Aircraft Establishment Westland Aircraft
Country of origin	United Kingdom
Size
Height	13 metres (43 ft)
Diameter	2 metres (6 ft 7 in)
Mass	18,130 kilograms (40,000 lb)
Stages	Three
Capacity
Payload to 220 km LEO	135 kilograms (300 lb)
Payload to 500 km LEO	102 kilograms (220 lb)
Launch history
Status	Retired
Launch sites	Woomera LA-5B
Total launches	4
Successes	2
Failures	2
Maiden flight	27 June 1969
Last flight	28 October 1971
First Stage
Engines	Gamma 8
Thrust	256.4 kilonewtons (57,600 lbf)
Specific impulse	265 sec
Burn time	131 seconds
Fuel	RP-1/HTP
Second Stage
Engines	Gamma 2
Thrust	68.2 kilonewtons (15,300 lbf)
Specific impulse	265 sec
Burn time	116 seconds
Fuel	RP-1/HTP
Third Stage - Waxwing
Engines	1 Solid
Thrust	27.3 kilonewtons (6,100 lbf)
Specific impulse	278 sec
Burn time	55 seconds
Fuel	Solid

Black Arrow, officially capitalised BLACK ARROW, was a British satellite carrier rocket. Developed during the 1960s, it was used for four launches between 1969 and 1971. Its final flight was the first successful orbital launch to be conducted by the United Kingdom, and placed the Prospero satellite into low Earth orbit.
Black Arrow originated from studies by the Royal Aircraft Establishment for carrier rockets based on the Black Knight rocket,with the project being authorised in 1964. It was initially developed by Saunders-Roe, and later Westland Aircraft as the result of a merger.
Black Arrow was a three-stage rocket, fuelled by RP-1 paraffin and high test peroxide, a concentrated form of hydrogen peroxide.It was retired after only four launches in favour of using American Scout rockets, which the Ministry of Defence calculated to be cheaper than maintaining the Black Arrow programme.

Contents 1 Development 2 Vehicle 3 Launches 4 Cancellation 5 See also 6 External links 7 References

Development

Black Arrow originated from a Royal Aircraft Establishment proposal for a rocket capable of placing a 144-kilogram (320 lb) payload into low Earth orbit, in order to test systems designed for larger spacecraft. In the autumn of 1964, the programme was authorised by Conservative Aviation Minister Julian Amery; however, following a general election in October, the incoming Labour government put the project on hold to reduce expenditure.
Following another election, the government approved the continuation of the programme with several modifications, including the reduction of the test programme from five to three launches. The first launch was set for 1968.
Most of the technology and systems used on Black Arrow had already been developed or flight-proven on the Black Knight rocket, or the Blue Steel missile.Black Arrow was designed to reuse as much technology from the earlier programmes as possible in order to reduce costs, and simplify the development process.Many senior staff of the Black Knight programme transferred directly to Black Arrow, including the Chief Missile Scientist, Roy Dommett, the Chief Design Engineer, Ray Wheeler and the Deputy Chief Engineer, John Underwood.
Initial development was conducted by Saunders-Roe, which merged into Westland Aircraft in 1964. Westland was subsequently the prime contractor for the Black Arrow, and assembled the first and second stages at East Cowes on the Isle of Wight. Bristol Siddeley produced the first and second stage engines at a factory in Ansty, Warwickshire. The engines were test fired at the factory before being shipped to the Isle of Wight, where they were integrated into the rocket and the first stage engines were fired again at High Down.Bristol Aerojet produced the third stage in Somerset, while the Explosives Research and Development Establishment produced its solid propellent in Waltham Abbey, Essex. The Rocket Propulsion Establishment, based in Westcott, Buckinghamshire, was responsible for the design and integration of the stage.
The name Black Arrow came from the Ministry of Supply policy of assigning designations consisting of a colour and a noun, unofficially known as Rainbow Codes, to research programmes conducted by the Armed Forces.

Vehicle

Cutaway diagram, showing the positions of fuel and oxidiser tanks, engines, and the third stage inside the fairing.

The first and second stages of the Black Arrow were fuelled by RP-1 paraffin, burnt using high test peroxide as an oxidiser. Due to the optimum mixture ratio being about 7 a larger oxidiser tank was required compared to many contemporary launch systems.The oxidiser tanks were located below the fuel tanks, following the practice of putting the more dense propellent at bottom in order to lower the centre of gravity and make the rocket easier to control.This arrangement had been pioneered by Germany and the United States, whereas the Soviet Union had placed oxidiser tanks above fuel tanks, making it easier for the lower tank to be filled first.
Thrust vectoring was used to provide attitude control on the first two stages.The eight first stage combustion chambers were arranged in pairs which could gimbal either way along one axis.Two of the pairs were arranged perpendicular to the other two, and when all four pairs were used together, they provided roll, pitch and yaw control. The second stage had two combustion chambers, which could gimbal along two axes, providing the same level of control. During a coast phase after second stage cut-off, the rocket was controlled by a reaction control system. The third stage did not have an attitude control system, and was instead spin-stabilised.
The first stage was powered by a single Gamma 8 engine, which burned for 127 seconds. The Gamma 8 was an eight-chamber engine, derived from the Gamma 301 engine used on the Black Knight. It was 6.9 metres (23 ft) long, and had a diameter of 2 metres (6 ft 7 in), the same diameter as the French Coralie. Coralie was used as the second stage of the Europa rocket, and the decision to give Black Arrow the same diameter as Coralie was taken in order to make it compatible with Blue Streak, which was used as the first stage of Europa. This would have allowed Black Arrow's payload capacity to have been increased, and would also have allowed Britain to use the first stage of Black Arrow as a backup to the Coralie. For this reason, all dimensions in the original specification were given in imperial units except the first stage diameter, which was given in metres.
The first and second stages were connected by an interstage structure containing four Siskin IB separation and ullage motors, which separated and ignited seven seconds after the first stage had cut off.The interstage separated from the second stage six seconds later. The second stage, which was 2.9 metres (9 ft 6 in) long and measured 1.37 metres (4 ft 6 in) in diameter, was powered by a two-chamber Gamma 2 enginewhich ignited shortly after the separation motors, and continued to burn for 123 seconds.Three minutes after launch, during the second stage burn, the payload fairing separated.

The first two stages and open payload fairing of R4 on display at the Science Museum in London

About 257 seconds into the flight, the second stage cut off, and the rocket entered a coast phase to apogee.Immediately after cut-off, the second stage attitude control system was pressurised. During the coast the correct orientation for third stage separation was maintained by means of the attitude control system.Towards the end of the coast period, the third stage was be spun up to a rate of 3 hertz (180 rpm) by means of six Imp rockets.Five seconds later, the third stage separated, and following ten more seconds of coasting, it ignited. The third stage was a Waxwing solid rocket motor, which burned for 55 seconds.
Just over a minute after the third stage had burned out, the payload was released, and gas generators were used to push the spacecraft and spent upper stage apart.The delay between burnout and separation was intended to reduce the risk of recontact between the upper stage and payload due to residual thrust. Despite this, following spacecraft separation on the R3 launch, the upper stage collided with the Prospero satellite,damaging one of the spacecraft's communications antennae; however the spacecraft was still able to successfully complete its mission. On the R3 launch, the ascent took 710 seconds (11.8 min) from liftoff to spacecraft separation.
Although none was ever built, several derivatives of Black Arrow were also proposed, as ways of increasing its payload capacity.One proposal added eight Raven solid rocket motors from the Skylark programme to the first stage as booster rockets.Another suggestion was to mount the entire rocket atop a Blue Streak missile,while a third proposal involved replacing the Gamma engines with the more powerful Larch.

Launches

The colour scheme used on all flights except R0, with stripes on the first stage for identification, and a coloured fairing to increase visibility.

Four Black Arrows were launched between 1969 and 1971. The first two launches were demonstration flights, with battleship third stages and a boilerplate payload. On the first flight an electrical fault caused a pair of first stage combustion chambers to pivot back and forth.Before it cleared the launch pad, the rocket was rolling erratically, and about a minute later it began to disintegrate. After the first stage engine failed, and the rocket began to fall back to earth, it was destroyed by range safety.The second launch was successful. The first all-up launch on 2 September 1970 was the third launch of the Black Arrow, and Britain's first attempt to launch a satellite. The launch failed due to a leak in the second stage oxidiser pressurisation system, which caused it to cut out early. The third stage fired, but the rocket did not reach orbit, and re-entered over the Gulf of Carpentaria. The fourth launch successfully orbited the Prospero satellite, making the United Kingdom the sixth nation to place a satellite into orbit by means of an indigenously developed carrier rocket. The satellite, also known as X-3, was named Prospero after the character Prospero in Shakespeare's The Tempest. The name was chosen as a reference to events in the play, in which Prospero, a sorcerer, gives up his powers.Prior to the cancellation of the Black Arrow programme, the satellite was to be named after Puck from A Midsummer Night's Dream.
All four launches were conducted from Launch Area 5B at the Woomera Prohibited Area in Australia, which had previously been used as a test site for the Black Knight rocket. During the development programme, launch sites in Barbados, Uist and Norfolk were also considered. The launch sites at Uist and Norfolk were rejected because the former was too remote, while there was a risk that a rocket launched from the latter might drop spent stages on an oil rig in the North Sea.

Serial number	Launch date/time (GMT)	Payload	Outcome	Remarks
R0	28 June 1969, 22:58	None	Failure	Suborbital test of first and second stages, thrust vectoring failed
R1	4 March 1970, 21:15	None	Successful	Suborbital test of first and second stages
R2	2 September 1970, 00:34	Orba	Failure	Second stage failed to pressurise
R3	28 October 1971, 04:09	Prospero	Successful	Successfully reached Earth orbit
R4	Not launched			Preserved at the Science Museum in London

Cancellation

Black Arrow R4 on display in the Science Museum, with the stages and fairing separated, and a mockup of the Prospero satellite

The Minister of State for Trade and Industry, Frederick Corfield, announced the cancellation of the Black Arrow project in the House of Commons on 29 July 1971. As the R3 rocket had already been shipped to the launch site, the second stage having arrived three days earlier, permission was given for it to be launched.
The programme was cancelled on economic grounds, as the Ministry of Defence decided that it would be cheaper to use the American Scout rocket, which had a similar payload capacity, for future launches.Prior to the cancellation of Black Arrow, NASA had offered to launch British payloads for free; however, this offer was withdrawn following the decision to cancel Black Arrow.
The final Black Arrow to be completed was R4, which did not fly, and is preserved in the Science Museum, London, along with the flight spare for the Prospero satellite.A replica of the Black Arrow rocket stands in the Rocket Park at Woomera. In addition, the remains of the first stage of Black Arrow R3 were recovered from the Anna Creek cattle station and are displayed in the William Creek Memorial Park.

The first stage of Black Arrow R3, on display at William Creek following its return to Earth

The launch facilities at Woomera were demolished within a year of the final flight,and half of the engineers who had worked on the programme were laid off.The X-4 satellite, which had been manifested for launch by Black Arrow R4, was eventually launched on 9 March 1974, by an American Scout D-1 rocket flying from Space Launch Complex 5 at the Vandenberg Air Force Base in California.
As of 2011, the United Kingdom is the only country to have successfully developed and then abandoned a satellite launch capability.All other countries that have developed such a capability have either retained it through their own space programme or, in the case of France, through its involvement in the Ariane programme.