 A mockup of the Black Arrow in therocket park at Woomera. | |
| Function | Carrier rocket |
|---|---|
| Manufacturer | |
| Country of origin | United Kingdom |
| Size | |
| Height | 13 metres (43 ft)[1] |
| Diameter | 2 metres (6 ft 7 in)[2] |
| Mass | 18,130 kilograms (39,970 lb)[1] |
| Stages | 3 |
| Capacity | |
| Payload toLEO[altitude and inclination needed] | |
| Altitude | 220 km (140 mi) |
| Mass | 135 kilograms (298 lb)[2] |
| Payload to LEO[altitude and inclination needed] | |
| Altitude | 500 km (310 mi) |
| Mass | 102 kilograms (225 lb)[2] |
| Launch history | |
| Status | Retired |
| Launch sites | WoomeraLA-5B |
| Total launches | 2 (+2 suborbital) |
| Success(es) | 1 (+1 suborbital) |
| Failure | 1 (+1 suborbital) |
| First flight | 27 June 1969[1] |
| Last flight | 28 October 1971[1] |
| First stage | |
| Powered by | Gamma 8 |
| Maximum thrust | 256.4 kilonewtons (57,600 lbf) |
| Specific impulse | 265 seconds (2.60 km/s) |
| Burn time | 131 seconds |
| Propellant | RP-1/HTP |
| Second stage | |
| Powered by | Gamma 2 |
| Maximum thrust | 68.2 kilonewtons (15,300 lbf) |
| Specific impulse | 265 seconds (2.60 km/s) |
| Burn time | 116 seconds |
| Propellant | RP-1/HTP |
| Third stage –Waxwing | |
| Powered by | 1solid |
| Maximum thrust | 27.3 kilonewtons (6,100 lbf) |
| Specific impulse | 278 seconds (2.73 km/s) |
| Burn time | 55 seconds |
| Propellant | Solid |
Black Arrow, officially capitalisedBLACK ARROW,[3] was a Britishsatelliteexpendable launch system.
Black Arrow originated from studies by theRoyal Aircraft Establishment for carrier rockets based on the earlierBlack Knight rocket;[4] the project was authorised by the British government in late 1964. Development of Black Arrow was largely performed by the prime contractor, the British aerospace companySaunders-Roe, and later undertaken byWestland Aircraft as the result of a merger. Both the first and second stage engines were produced byBristol Siddeley at their factory inAnsty,Warwickshire. Assembly of the first and second stages was carried out atEast Cowes on theIsle of Wight. Once manufactured, each Black Arrow vehicle was transported by ship to Australia prior to being launched from theRAAF Woomera Range Complex.
Black Arrow was a three-stage rocket, fuelled byRP-1paraffin (kerosene) andhigh-test peroxide, a concentrated form ofhydrogen peroxide (85% hydrogen peroxide + 15% water).[5] While the first two stages featuredthrust vectoring to provide attitude control,[4] the third stage did not have an attitude control system, and instead relied uponspin stabilization along with areaction control system. The first stage was designed to be compatible withBlue Streak, as well as to be interchangeable withCoralie.[6] Furthermore, several derivatives of Black Arrow were proposed to provide for increased payload capacity.
A total of four launches of Black Arrow were performed between 1969 and 1971, the first two being demonstration flights to prove the launcher's capabilities. While the first and third flights were failures, the second and fourth flights were successful. Black Arrow's final flight placed theProspero satellite intolow Earth orbit, making it the first and only successful orbital launch to be conducted by the United Kingdom.[2] British officials decided to discontinue the programme in favour of using AmericanScout rockets instead, theMinistry of Defence having calculated this option to be cheaper than continuing with Black Arrow.[7] The final Black Arrow to be completed, which never flew, has been preserved intact at theScience Museum, London, along with the flight spare for the Prospero satellite.
Black Arrow originated from a Royal Aircraft Establishment proposal for a rocket capable of placing a 317-pound (144 kg) payload intolow Earth orbit,[altitude and inclination needed] in order to test systems designed for larger spacecraft.[8] In the autumn of 1964, the programme was authorised byConservativeAviation MinisterJulian Amery.[9] Then, following ageneral election in October, the incomingLabour government put the project on hold to reduce expenditure.[10] Following anotherelection, the British government approved the continuation of the programme with several modifications, including the reduction of the test programme from five to three launches. The maiden launch was set for 1968.[11][12]
Initial development was conducted by the British aerospace manufacturerSaunders-Roe, which merged intoWestland Aircraft in 1964.[13] Westland was subsequently the prime contractor for the Black Arrow, and assembled the first and second stages atEast Cowes on theIsle of Wight, later testing the rockets from the 1950s up until the rocket launch on 28 October 1971.[14] The British powerplant specialistBristol Siddeley produced the first and second stage engines at a factory inAnsty, Warwickshire.[15] 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 atHigh Down.[16]Bristol Aerojet produced the third stage inSomerset, while theExplosives Research and Development Establishment produced itssolid propellant inWaltham Abbey,Essex.[4] TheRocket Propulsion Establishment, based inWestcott, Buckinghamshire, was responsible for the design and integration of the stage.[4][17]
The majority of the technology and systems used on Black Arrow had already been developed or flight-proven on theBlack Knight rocket, or theBlue Steel missile.[4] 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.[18] Many senior staff of the Black Knight programme transferred directly to Black Arrow, including the Chief Missile ScientistRoy Dommett, the Chief Design EngineerRay Wheeler, and the Deputy Chief Engineer John Underwood.[19] Despite this effort, the programme encountered more difficulties and greater costs than had originally been anticipated.[20] This outcome was in no small part due to the austere budget of £3 million per year.[12][21]
The nameBlack Arrow came from theMinistry of Supply policy of assigning designations consisting of a colour and a noun, unofficially known asRainbow Codes, to research programmes conducted by theArmed Forces.[3][22] Despite this naming convention, the programme was officially a civilian venture.[23] It was unofficially nicknamed the "Lipstick Rocket", as the fairing, which was painted bright red for visibility, made the rocket resemble a tube oflipstick.[24]
Black Arrow was a relatively compact launch vehicle, being particularly slender as well as possibly being the shortest rocket ever to place a satellite into orbit.[25] The first and second stages of the Black Arrow were fuelled by RP-1 paraffin (kerosene), burnt using high test peroxide as anoxidiser.[5][26] Due to the optimum mixture ratio being about 7, a larger oxidiser tank was required compared to many contemporary launch systems.[27] The oxidiser tanks were located below the fuel tanks, following the practice of putting the more dense propellant at the top in order move thecentre of gravity higher and make the rocket more stable, when in flight,[28] and thus easier to control.[4] This arrangement had been pioneered by Germany and the United States, whereas theSoviet Union had placed oxidiser tanks above fuel tanks, making it easier to fill the lower tank first.[29]
Thrust vectoring was used to provide attitude control on the first two stages.[4] The eight first stagecombustion chambers were arranged in pairs which couldgimbal either way along one axis.[4] Two of the pairs were arranged perpendicular to the other two, and when all four pairs were used together, they providedroll, pitch, and yaw control.[4] The second stage had two combustion chambers, which could gimbal along two axes, providing the same level of control. During acoast phase after second stage cut-off, the rocket was controlled by areaction control system.[4] The third stage did not have an attitude control system, and was insteadspin-stabilised.[2] The guidance system used was derived from that of the cancelledBAC TSR-2bomber.[25]
The first stage was powered by a singleGamma 8 engine, which burned for 127 seconds.[2] The Gamma 8 was an eight-chamber engine, derived from the Gamma 301 engine used on the Black Knight.[30] It was 6.9 metres (23 ft) long, and had a diameter of 2 metres (6 ft 7 in), the same diameter as the FrenchCoralie.[2] Coralie was used as the second stage of theEuropa rocket. Black Arrow had the same diameter as Coralie to make it compatible withBlue Streak, which was used as the first stage of Europa.[6] 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.[31] For this reason, all dimensions in the original specification were given inimperial units except the first stage diameter, which was given inmetric units.[6]
The first and second stages were connected by aninterstage structure containing fourSiskin IBseparation andullage motors, which separated and ignited seven seconds after the first stage had cut off.[4][32] 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 engine[33] which ignited shortly after the separation motors, and continued to burn for 123 seconds.[2] Three minutes after launch, during the second stage burn, thepayload fairing separated.[2]
About 257 seconds into the flight, the second stage cut off, and the rocket entered a coast phase toapogee.[2] 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.[2] Towards the end of the coast period, the third stage was spun up to a rate of 3 hertz (180 rpm) by means of sixImp rockets.[2] Five seconds later, the third stage separated,[4] and following ten more seconds of coasting, it ignited. The third stage was aWaxwing solid rocket motor, which burned for 55 seconds.[2]
Just over a minute after the third stage had burned out, the payload was released, andgas generators were used to push the spacecraft and spent upper stage apart.[2] The delay between burnout and separation was intended to reduce the risk ofrecontact 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,[2] damaging one of the spacecraft's communications antennae.[34] Despite this, the spacecraft was still able to complete its mission successfully.[34] On the R3 launch, the ascent took 710 seconds (11.8 min) from liftoff to spacecraft separation.[2]
Although none were ever built, several derivatives of Black Arrow were also proposed, typically focused upon increasing its payload capacity.[35] In its standard configuration, Black Arrow was not capable of launching some contemporary satellites up to a sufficient altitude to achievegeostationary orbit.[36] Accordingly, one proposal was to add eight Raven solid rocket motors from theSkylark programme to the first stage asbooster rockets.[4] Another suggestion was to mount the entire rocket atop a Blue Streak missile,[37][38] while a third proposal involved replacing the Gamma engines with the more powerfulLarch.[4]
Four Black Arrows were launched between 1969 and 1971.[39] The first two launches were demonstration flights, withbattleship third stages and aboilerplate payload. On the maiden flight, an electrical fault caused a pair of first stage combustion chambers to pivot back and forth.[40] 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 byrange safety.[41][42] This initial failure was a considerable blow to the programme, particularly as there were insufficient financial reserves to accommodate a second unsuccessful launch. The second Black Arrow vehicle was returned to Britain for inspection and fixes ahead of the next launch.[43]
The second launch, performed on 4 March 1970, was entirely successful.[43] On 2 September 1970, the third launch of the Black Arrow took place; it was the first all-up launch as well as Britain's first attempt to launch a satellite. This 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, andre-entered over theGulf of Carpentaria.[44] An extensive programme review was conducted in the aftermath of the third launch, which determined that Black Arrow's design had no fundamental flaws and that only minor modifications were required.[45]
The fourth launch, performed on 28 October 1971, successfully orbited theProspero (before the R2 mission, it was named Puck) satellite, making the United Kingdom thesixth 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 characterProspero inShakespeare'sThe Tempest. The name was chosen as a reference to events in the play, in which Prospero, a sorcerer, gives up his powers.[46] Prior to the cancellation of the Black Arrow programme, the satellite was to be named afterPuck fromA Midsummer Night's Dream.[5]
All four launches were conducted fromLaunch Area 5B at theRAAF Woomera Range Complex in Australia, which had previously been used as a test site for theBlack Knight rocket.[47] During the development programme, launch sites inBarbados,Uist, andNorfolk 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 anoil rig in theNorth Sea.[25][48]
| Serial number | Launch date/time (GMT) | Payload | Outcome | Remarks |
|---|---|---|---|---|
| R0 | 28 June 1969, 22:58[1] | None | Failure | Suborbital test of first and second stages, thrust vectoring failed[41] |
| R1 | 4 March 1970, 21:15[1] | None | Success | Suborbital test of first and second stages |
| R2 | 2 September 1970, 00:34[1] | Orba[1] | Failure | Second stage failed to pressurise |
| R3 | 28 October 1971, 04:09[49] | Prospero[49] | Success | Successfully reached Earth orbit |
| R4 | Not launched | Preserved at theScience Museum inLondon[4] | ||
TheMinister of State for Trade and Industry,Frederick Corfield, announced the cancellation of the Black Arrow project in theHouse of Commons on 29 July 1971.[50][45] Britain would instead focus its space activities on building satellites and rely on foreign launch vehicles.[51] 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.[2]
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.[7][52][53] 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.[2]
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 theProspero satellite.[54][55] A replica of the Black Arrow rocket stands in theRocket Park at Woomera. In addition, the remains of the first stage of Black Arrow R3 were recovered from theAnna Creek cattle station and were displayed in theWilliam Creek Memorial Park.[56] Due to weather and vandalism related damage, the first stage was returned to the United Kingdom in an initiative led bySkyrora to preserve the artefact.[57] It was displayed inPenicuik, Scotland, in early 2019; as of Spring 2024, the rocket is on loan to theFarnborough Air Sciences Trust Museum.[58][59]
The launch facilities at Woomera were demolished within a year of the final flight,[4] and half of the engineers who had worked on the programme were laid off.[41] TheX-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 fromSpace Launch Complex 5 at theVandenberg Air Force Base inCalifornia.[60]
As of 2024, the United Kingdom is the only country to have successfully developed and then abandoned a satellite launch capability.[61][59] All other countries that have developed such a capability have retained it either through their own space programme or, in the case of France, through its involvement in theAriane programme.[61] However, a second British launch vehicle, theSkyrora, is currently under development.[62]
Black Arrow rockets | ||
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