Skylark was a family of British sounding rockets. It was operational between 1957 and 2005. Development of the Skylark begun during the early 1950s at the Royal Aircraft Establishment (RAE), which approached the Royal Society with an offer for it to carry scientific experiments. During early 1955, the British government agreed to provide £100,000 to support the programme's operations for four years. Development of the Skylark, initially known as the CTV.5 Series 3, was pursued at a rapid pace, with hopes that initial launches could take place during the latter half of 1956. On 7 April 1956, the existence of the Skylark rocket was publicly revealed under the early name of Gassiot vehicle. Launch facilities were established at the existing Woomera missile range in Australia; the Skylarks were produced in Britain and flown to Australia for final assembly, testing, and launching. The Skylark was first launched on 13 February 1957; the first scientific mission occurred during April 1958, quickly becoming regarded as a valuable platform for various fields of research. The vast majority of launches would be performed from Woomera, although other launch sites would later be used at sites across Europe and South America. The British government opted to terminate its support of the programme in 1977, with responsibility for Skylark being turned over to British Aerospace. It continued to be operated for decades more. The 441st and final launch of the Skylark took place from Esrange, Sweden, on 2 May 2005. Launches had been carried out from various purposes, with some military missions being flown, users extended far beyond the UK to include NASA, the European Space Research Organisation (ESRO), and German and Swedish space organizations.
History
Development The origins of the Skylark can be traced back to decisions made in the aftermath of the Second World War. Unlike some powers, the United Kingdom had not opted to immediately proceed with work on long-range rocketry; however, the Ministry of Supply did work on defensive guided weaponry, leading to the arrival of surface-to-air missiles such as the Bloodhound during the 1950s. To conduct these programmes, the ministry developed a series of test missiles for research and development. During May 1953, amid the preparations for a major conference in Oxford on rocket-based exploration of the upper atmosphere, the Ministry of Supply approached the Gassiot Committee of the Royal Society with an offer of using ministry rockets for scientific research. This offer, while positively received, was quickly realised to far exceed what would be affordable to the universities. During February 1954, a group of scientists enthusiastically responded to a closed briefing on a Royal Aircraft Establishment (RAE) project, the CTV.5 Series 3 rocket (which would later adopt the name Skylark). The CTV series of rockets had originally been used to investigate aerodynamic control of missiles, yet the Skylark was stated to be capable of carrying a payload of 100 lb to an altitude of 200 km (124 mi). The Royal Society promptly approached HM Treasury with a request for £100,000 to fund upper atmospheric rocket research over the course of four years. There was considerable interest in exploring the ionosphere, which was relatively unknown at that time, and Skylark would be a revolutionary tool for its study. During April 1955, following the approval of funding, the research programme formally commenced; roughly half of the £100,000 was spent on the vehicles themselves, while the remainder covered the costs of scientific instruments and technical staff. Various university groups were responsible for the design and construction of the scientific instruments carried, as well as post-mission analysis; all other aspects were the responsibility of the Ministry of Supply. A subcommittee of the Gassiot Committee coordinated the overall programme. In addition to its scientific role, Skylark was also to serve a military purpose, being available to the RAE's research programme, including in the development of ballistic missiles; in return, the RAE provided considerable assistance in the rocket's design, manufacture, preparation, and firing. Numerous RAE personnel were allocated to the Skylark initiative. A relatively ambitious target date for the first launch was set for the summer of 1956 during the International Geophysical Year, necessitating development to be completed in little over a year. Additional support for the Skylark programme was sourced from the Rocket Propulsion Establishment (RPE) at Westcott with the development and testing of the Raven 1 rocket engine. On 7 April 1956, the existence of the Skylark rocket was publicly revealed under the early name of Gassiot vehicle. Even before this announcement, it had been decided that Skylark would be fired from the Woomera rocket range in Australia. While work did proceed at a fast pace on the project, an ignition problem encountered during the RPE's proof testing forced the postponement of the first launch past a November 1956 slot and, partially due to the Woomera's range's closure for Christmas, was delayed until the following year. On 13 February 1957, the Skylark performed its first launch from Woomera; for this initial test flight, it carried no experimental payload save for RAE test instrumentation to monitor the rocket's performance. It was the first long range vehicle to be launched from Woomera.
Operations During April 1958, scientific use of the Skylark commenced, marking the programme's attainment of true operational status. Unlike the majority of missile/rocket programmes, which would only temporarily be based at Woomera until they matured, Skylark continued to operate at Woomera as its long term home. This arrangement necessitated an international supply chain between Britain and South Australia; early Skylarks were transported by plane, along with a kit of parts that were locally assembled by a mostly Australian workforce. Once assembled, the rockets would be transported a further 270 miles to the actual range for roughly two weeks of final preparation ahead of launching. After multiple rounds of testing, the rocket would be mounted on a trailer and taken to the launch platform, usually two days prior to the launch date; the launch itself was overseen by Australian Weapons Research Establishment personnel from an underground control room at the edge of the concrete apron.
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