Attention now turned to Thor-Able 127 and The next six Thor-Able flights were suborbital tests for the Air Force (23 January, 28 February, 21 March, 8 April, 20 May, and 11 June 1959). There were two separate problems with the pumps. Thor 114 was destroyed by Range Safety 150 seconds into launch when the guidance system lost power and Thor 120's engine shut down slightly under two minutes after liftoff.
Operation Dominic I. The guidance system tried to compensate, but the resulting structural loads exceeded the strength of the missile tankage. Burner 2 used a Thiokol Star 37B motor (TE-M-364-2). The last launch of a direct derivative of the Thor missile occurred in 2018 as the first stage of the final Delta II Modified bearing retainers were not installed. The third Thor launch (Missile 103) exploded four minutes before the planned launch after a defective valve allowed LOX tank pressure to build up to unsafe levels.
Main engine burn time was almost 2.5 minutes, boosting the missile to a speed of 14,400 ft/s (4,400 m/s). United States tri-service rocket designations post-1963 Members of the By 1969, the Thor core was being used regularly both in Delta vehicles and in the USAF Standard Space Launch Vehicle (SLV-2), with thrust augmentation and a variety of upper stages. Page 229-241.
The Thor-Able was an American expendable launch system and sounding rocket used for a series of re-entry vehicle tests and satellite launches between 1958 and 1960.It was a two stage rocket, consisting of a Thor IRBM as a first stage and a Vanguard-derived Able second stage. Unfortunately, Wickie was no luckier than her predecessors when recovery crews once again failed to locate the capsule after splashdown, but telemetry data confirmed the mouse's survival from liftoff through reentry and proved comprehensively that living organisms could survive space travel. Another 23 Thor missile tests were carried out during 1959, with only one failure, when Missile 185 on 16 December, the second RAF launch, broke up due to a control malfunction. Thor was first used as a launch vehicle during the testing program of the warhead reentry vehicle for the The Able stage from the Atlas reentry vehicle tests was upgraded to become the Able I with a third stage consisting of an unguided Altair X-248 solid-fuel rocket motor. A film of prelaunch preparations showed crews dragging a LOX filler hose through a sandy area, and it was that debris had entered the LOX, causing the failure of a valve. Eventually though, they became nervous about it exploding or pitching over, so the destruct command was sent around 50 seconds into launch. No telemetry equipment was included on this missile, with the resulting mass savings allowing a total range of 1,500 miles (2,400 km). The Thor-Able vehicle had a stronger airframe than the standard Thor IRBM and had the inertial guidance system replaced by a radio guidance package mounted on the Able stages. It was erected at LC-17B and underwent several practice propellant loading/unloading exercises, a static firing test, and a month-long delay while a defective relay was replaced. The first was the discovery during testing at Huntsville that the lubricant oil tended to foam at high altitude as the air pressure decreased. High-altitude wind caused debris to land in the town of Orcutt near the base. Ten minutes into its flight the missile reached an altitude of 280 miles (450 km), close to the The Thor was initially deployed with a very blunt conical G.E. All of these were successful except the first one, which failed to stage due to an electrical problem and fell into the Atlantic Ocean.
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