. . . . . . . . . "1.01"^^ . . . . . . "22000.0"^^ . . "Retired"@en . "1"^^ . . . . . . "3831"^^ . . . "1"^^ . . . . "1.01"^^ . "Retired" . . . . . . . "1962-03-01"^^ . . "Scout X-1A was an American sounding rocket which was flown in 1962. It was a five-stage derivative of the earlier Scout X-1, with an uprated first stage, and a upper stage. The Scout X-1A used an first stage, instead of the earlier used on the Scout X-1. The second, third and fourth stages were the same as those used on the Scout X-1; a Castor 1A, Antares 1A and Altair 1A respectively. The fifth stage was the NOTS-17 solid rocket motor, which had been developed by the Naval Ordnance Test Station. The Scout X-1A was launched on its only flight at 05:07 GMT on 1 March 1962. It flew from Launch Area 3 of the Wallops Flight Facility. The flight carried an atmospheric re-entry experiment to an apogee of 214 kilometres (133 mi), and was successful. Following this, the Scout X-1A was replaced by the Scout X-2."@en . . . . . . . . . . . . "1120093094"^^ . "17000.0"^^ . . . . "Scout X-1A was an American sounding rocket which was flown in 1962. It was a five-stage derivative of the earlier Scout X-1, with an uprated first stage, and a upper stage. The Scout X-1A used an first stage, instead of the earlier used on the Scout X-1. The second, third and fourth stages were the same as those used on the Scout X-1; a Castor 1A, Antares 1A and Altair 1A respectively. The fifth stage was the NOTS-17 solid rocket motor, which had been developed by the Naval Ordnance Test Station."@en . "United States"@en . . "0"^^ . . . . "0"^^ . "22.0"^^ . . . "23314803"^^ . . . "1"^^ . "Scout X-1A"@en . "17000.0"^^ . "1"^^ . . . "17000000.0"^^ . . . . . . . . "Five"@en . .