Aberporth Credit: © Mark Wade |
Zucker, his backer, and selected press representatives met on a hilltop on Sussex Downs. After a first successful test launch without payload, two launches were made with postal covers. The observers guessed the rockets went as high as 400 to 800 m. Banner headlines the next day announced 'The First British Rocket Mail' and carried Zucker's claim that soon he would inaugrate regular one minute rocket post service between Dover and Calais.
Zucker announced a demonstration firing of his rocket over 1600 m of water between the town of Harris and the Isle of Scarp. Government officials watched as the rocket exploded, blowing the burning payload of postal covers all over the beach. The British found Zucker to be a 'threat to the income of the post office and the security of the country'. He was deported to Germany, where he was immediately arrested by the Germans on suspicion of espionage or collaboration with Britain.
Third and final launch in Project Backfire, with allied observors. Glushko, Sokolov, Pobedonostsev; Korolev and Gaidukov kept outside fence; Von Karman, Merrill, Seifert, Pickering from US. The launch was successful and the missile reached an altitude of 90 km.
A paper read to the British Interplanetary Society by H. E. Ross described a manned lunar landing mission which would require a combination of the earth orbit and lunar orbit rendezvous techniques. Three spacecraft would be launched simultaneously into earth orbit, each carrying a pilot. After rendezvous, the crew would transfer to ship A, which would refuel from ships B and C. Ship C would be discarded completely, but ship B would be fueled with the surplus not needed by A. The spacecraft would then be fired into a translunar trajectory. Upon reaching the vicinity of the moon, the spacecraft would go into lunar orbit, detach fuel tanks, and descend to the lunar surface. To return to earth, the spacecraft would rendezvous with the fuel tanks, refuel, and fire into a transearth trajectory. On approaching the earth, the spacecraft would rendezvous with ship B, the crew would transfer to ship B, and descend to earth. The ability to rendezvous in space was seen to be the essential element of such a project. The total payload weight at launch would be 1,326 tons equally divided among the three ships as compared to 2.6 times this weight required for a direct ascent and return from the moon.
In a paper presented to the British Interplanetary Society, H. E. Ross described a manned satellite station in Earth orbit that would serve as an astronomical and zero-gravity and vacuum research laboratory. (Ross' bold suggestions also included schemes for a manned landing on the Moon and return to Earth through use of the rendezvous technique in Earth orbit and about the Moon.) Ross' suggested design comprised a circular structure that housed the crew of the space laboratory (numbering 24 specialists and support personnel) as well as telescopes and research equipment. The station, he suggested, could be resupplied with oxygen and other life-support essentials by supply ships launched every three months.
Arthur C. Clarke's The Exploration of Space was first published in England in 1951, and became a US Book of the Month Club selection the following year. The book included an alternative to the direct ascent technique: assembling or refueling the space vehicle in earth orbit before injection into translunar trajectory, to be followed, possibly, by rendezvous in lunar orbit with fuel tanker rockets launched from the earth.
British-American physicist mission specialist astronaut 1987-2013. Flew in space six times. Appointed Deputy Associate Administrator for Exploration Operations in 2004. 373 cumulative days in space. 6 spaceflights, 373.8 days in space. Flew to orbit on STS-45 (1992), STS-56, STS-63, STS-84, STS-103, Soyuz TMA-3.
The study called for a two-crew waverider spacecraft powered by a second stage atop a British Blue Streak rocket. The group leaders of this project were H R Watson of Armstrong Whitworth, and Dr W F Hilton of Hawker Siddeley. The spacecraft design was by T R F Nonweiler.
American space tourist, 2007-2008. Son of astronaut Owen Garriott, raised in Nassau Bay, Texas. Sold first computer game at 16; made millions in computer games. Paid $30 million for a flight to the International Space Station. 1 spaceflight, 11.9 days in space. Flew to orbit on Soyuz TMA-13 (2008).
British Aircraft Corporation study of 1964-1965 for winged reuseable space shuttle using the 'triamese' concept - reduced costs by use of two boosters nearly identical to the orbiter vehicle. The components were lifting bodies with a configuration similar to the US HL-10 vehicle.
Skynet IA, the first of two Skynet military communications satellite built for the United Kingdom by the Philco-Ford Corporation, was launched from Cape Canaveral aboard a NASA Long Tank Thrust Augmented Thor/Delta (DSV-3L). The satellite was turned over to the United Kingdom on 30 January 1970, providing the United Kingdom with its first operational military communications satellite system. The Skynet satellites were designed to be usable with the Initial Defense Satellite Communication System (IDSCS) satellites of the United States. Over Indian Ocean. Military communications. Previously registered by the United States in A/AC.105/INF.220: 1969-101A, orbital data 276 x 36716 km x 28.0 deg, category C. Positioned in geosynchronous orbit over the Indian Ocean at 41 deg E in 1969-1972?; ??? 1972-1977; over the Americas at 100-110 deg W in 1977-1998 As of 26 August 2001 located at 104.51 deg W drifting at 0.015 deg W per day. As of 2007 Mar 9 located at 106.94W drifting at 0.015W degrees per day.
The second of two British Skynet I communication satellites (Skynet B) was launched from Cape Canaveral for U.S. Air Force and United Kingdom aboard a NASA Long Tank Thrust Augmented Thor/ Delta (DSV-3M) space booster. The spacecraft was placed in a transfer orbit prior to firing of the apogee kick motor that was to put it into a synchronous orbit over Kenya. Contact with Skynet B was lost during the firing of the apogee kick motor on 22 August and was not regained. The Skynet I satellites were part of the Initial Defense Satellite Communication System (TDSCS) program which was managed for the United Kingdom by SAMSO, with NASA providing launch vehicles and services. AKM failure left in unusable orbit. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).
A Thor-Delta launched from the Eastern Test Range lifted the second of two Skynet II (Skynet IIB) defense communications satellite for the United Kingdom into an elliptical transfer orbit. Two days later, a firing of the satellite's apogee boost motor placed the satellite in a near circular orbit prior to final positioning in a synchronous orbit over the Indian Ocean. The first Skynet II satellite, Skynet IIA, was lost in January 1974 due to a booster failure after launch from Cape Canaveral. Military communications. Positioned in geosynchronous orbit over the Indian Ocean at 50-55 deg E in 1975-1977; drifting As of 3 September 2001 located at 18.23 deg E drifting at 0.206 deg W per day. As of 2007 Feb 27 located at 54.93E drifting at 0.393E degrees per day.
University of Surrey research microsatellite. Radio science; also carried amateur radio package. Communication and geophysics research satellite. Launch time 1127 GMT. Also registered by the United States in ST/SG/SER.E/59, with category D and orbital parameters 95.3 min, 531 x 533 km x 97.5 deg. UoSAT-OSCAR 9 was launched piggyback with Solar Mesosphere Explorer satellite. Weight 52 kg. Box shaped 740 x 420 x 420 mm. Deployable gravity gradient boom. Firsts: First on-board computer (IHU - Integrated Housekeeping Unit) for battery and attitude management, remote control, and experiments. Built by the University of Surrey in the United Kingdom, UO-9 was UoSAT's first experimental satellite. It was a scientific and educational low-Earth orbit satellite containing many experiments and beacons but no amateur transponders. UO-9 was fully operational until it re-entered October 13, 1989 from a decaying orbit after nine years of service.
The project was reasonably well advanced (engine detailed design and mockup) by the time the British government withdrew further funding in the mid-1980's. HOTOL would have taken off horizontally, transition to pure rocket propulsion at Mach 5.0 - Mach 6.0. and ascend to orbit. A moderate re-entry profile would decrease the thermal loading constraints. HOTOL would return via a glide landing, to a landing on gear on a conventional runway.
University of Surrey experimental microsatellite. Built in only 6 months, UoSAT-2 carried the first modern digital store and forward (S&F) communications payload and a prototype CCD camera. Also performed magnetospheric studies. Launch time 1759 GMT. Still operational in 2000.
British military communications; 1 deg W. Military communications. Positioned in geosynchronous orbit at 1 deg W in 1989-1990; 53 deg E in 1990-1998 As of 4 September 2001 located at 60.05 deg E drifting at 2.136 deg W per day. As of 2007 Mar 10 located at 126.32E drifting at 2.116W degrees per day.
British DBS; 31 deg W. Direct broadcasting system. Expected operational life, 10 years. Owner/operator: British Satellite Broadcasting Ltd, The Marcopolo Building, Chelsea Bridge, Queenstown Rd, London SW8 4NQ. Positioned in geosynchronous orbit at 31 deg W in 1989-1993; 5 deg E in 1994-2000; 13 deg W in 2000. As of 31 August 2001 located at 12.98 deg W drifting at 0.008 deg W per day. As of 2007 Mar 9 located at 45.02W drifting at 3.908W degrees per day.
British military communications; 6 deg E. Military communications. Expected life approx 7 years. Owner/operator: Ministry of Defence, Main Building, Whitehall, London SW1A 2HB. Positioned in geosynchronous orbit at 6 deg E in 1990; 29 deg E in 1991; 65 deg E in 1991; 34 deg W in 1992-1999 As of 5 September 2001 located at 34.01 deg W drifting at 0.003 deg W per day. As of 2007 Mar 11 located at 63.46W drifting at 4.595W degrees per day.
University of Surrey experimental satellite. The first of Surrey Satellite Technology Ltd's modular microsatellites. Launched on the Ariane ASAP; carried an operational store and forward communications payload with extensive radiation monitoring experiments for SatelLife and Data Trax Inc (USA). Still operational in 2000. Owner/operator University of Surrey, Dept of Electronic and Electrical Engineering, Guildford, Surrey GU2 5XH.
Technology demonstration mission carrying transponder, solar cell, CCD camera technology experiments. Customer: University of Surrey/European Space Agency. Launched alongside UoSAT-3, the microsatellite operated perfectly for 2 days before a failure occured in the downlink. Owner/operator University of Surrey, Dept of Electronic and Electrical Engineering, Guildford, Surrey GU2 5XH. Box shaped 350 x 350 x 650 mm. Four solar panels and 6 m gravity gradient boom.
UK military communications; 1 deg W. United Kingdom military communications satellite. Owner/operator: UK Ministry of Defence. Expected operational life 10 years. Positioned in geosynchronous orbit at 1 deg W in 1990-1999 As of 3 September 2001 located at 0.97 deg W drifting at 0.002 deg E per day. As of 2007 Mar 10 located at 1.27W drifting at 0.000W degrees per day.
Skynet 4E was a SHF/UHF military communications satellite for the UK Ministry of Defense. Dry mass was 759 kg; it used a Thiokol Star 30 solid apogee motor. Stationed at 53 deg E. Positioned in geosynchronous orbit at 53 deg E in 1999. As of 5 September 2001 located at 52.91 deg E drifting at 0.000 deg W per day. As of 2007 Mar 11 located at 53.02E drifting at 0.005E degrees per day.
First launch of Russia's Dnepr launch vehicle, a converted R-36M2 ICBM. The Dnepr was launched from a silo. The third stage maneuvring bus (used on the ICBM for dispensing multiple warheads) placed UoSAT-12 into a 638 km x 652 km x 64.6 deg orbit. The third stage separated from the payload at 05:13 GMT and then made a burn into a 599 km x 1403 km x 64.6 deg orbit. UoSAT-12 was the first test of the Minibus platform, at 325 kg a larger spacecraft than earlier 50 kg Surrey UoSATs. It carried a mobile radio experiment (MERLION), a GPS receiver, and imaging cameras.
The SNAP-1 Surrey Nanosatellite Applications Platform was a 6 kg satellite with imager and propulsion. It was to test rendezvous techniques by formation flying with the Tsinghua satellite placed in orbit on the same launch. In October 2000 Surrey Satellite Technology Ltd (SSTL) released a picture of Tsinghua-1 taken in orbit by the SNAP-1 6.5 kg nanosatellite.
100th Ariane 4 launch. Communications satellite, stationed at 45 deg E. Europeon.Star FM1 was a Loral FS-1300 model with a launch mass of 4167 kg and a dry mass of 1717 kg. The satellite had two cruciform solar arrays. The Ariane booster placed it into a geostationary transfer orbit. Positioned in geosynchronous orbit at 45 deg E in 2000. As of 4 September 2001 located at 44.95 deg E drifting at 0.011 deg E per day. As of 2007 Feb 23 located at 44.97E drifting at 0.001W degrees per day.
STRV-1c and 1d were small satellites built by the DERA (former Royal Aircraft Establishment), Farnborough, England. Mass was around 95 kg each. STRV-1d carries an NRL Space Test Program experiment (S97-2), a camera, and technology and computer experiments.
The two small STRV cubes were then ejected from the Ariane EPS stage ASAP-5 secondary payload structure at 0141 GMT. STRV-1c and 1d were small satellites built by the DERA (former Royal Aircraft Establishment), Farnborough, England. Mass was around 95 kg each. STRV-1c performed accelerated life testing of new components and materials in the high radiation environment of geosynchronous transfer orbit.
Skynet 4F was a communications satellite for the UK Ministry of Defense, and the last of the venerable ECS (European Communications Satellite) class of satellites built by Astrium/Stevenage. It carried a Thiokol Star 30 apogee motor and its mass was 1489 kg full, 830 kg dry - a dry mass more than twice the first OTS. The spacecraft carried a total of eight transponders in the SHF-, UHF-, and S-bands to provide secure communications after parking over either 1 deg-E or 6 deg-W. Positioned in geosynchronous orbit at 6 deg E in 2001 As of 5 September 2001 located at 8.77 deg E drifting at 0.284 deg W per day. As of 2007 Mar 10 located at 6.01E drifting at 0.004E degrees per day.
Starchaser Industries (Hyde, England, UK) successfully tested a bi-propellant liquid rocket engine. "The liquid oxygen/kerosene powered system generated some 2,200 kilos of thrust for 15 seconds." The tests will continue for increasingly longer periods and will eventually reach "a full 3 tonnes of thrust".
Starchaser Industries (Hyde, England, UK) conducted two manned capsule drop tests from a C-123K transport aircraft at an altitude of 14,000 feet over the Red Lake Drop Zone in Kingman, Arizona, in order to practice landing the reusable craft. The main purpose of the tests was to ensure that the parachute, navigation, and landing systems function properly.
Third generation Disaster Monitoring Constellation. The three satellites were deployed on a single launch. DMC Imaging International was a Surrey Satellite spinoff which operated the DMC imaging satellites in collaboration with several developing countries. The satellites have the capability to return prompt imaging of areas in those countries affected by natural disasters. The SSTL-300S1 platform provided 45 degree fast slew off-pointing and was capable of acquiring multiple targets in one pass using multiple viewing modes. The high resolution imager on board the satellites was designed and manufactured by SSTL and provided 1 meter resolution in panchromatic mode, and 4 meter resolution in multispectral mode, with a swath width of 23.4km. The three satellites were phased 120 degrees apart around the same sun synchronous orbit with a 22:10 local time longitude of descending node sun synchronous orbit. This was acommplished using their on board propulsion systems in the three months after the launch. With off-pointing capability, the DMC3/TripleSat Satellite Constellation was able to target anywhere on Earth once per day.
In January 2017 it was reported that on this date a Trident missile launched from HMS Vengeance on the Atlantic Missile Range failed. The missile was said to have veered toward Florida before being destroyed by range safety. The government was said to have covered up the failure.