| 词条 | Scout X-1A |
| 释义 |
|function = Sounding rocket |manufacturer = Vought |country-origin = United States |height = {{convert|22|m}} |diameter = {{convert|1.01|m}} |mass = {{convert|17000|kg}} |stages = Five |family = Scout |status = Retired |sites = Wallops LA-3 |launches = 1 |success = 1 |fail = 0 |only = 1962-03-01 |stagedata = |type = Stage |stageno = First |name = Algol 1C |engines = 1 solid |thrust = {{convert|471|kN}} |SI = 236 sec |burntime = 40 seconds |fuel = Solid |type = Stage |stageno = Second |name = Castor 1A |engines = 1 solid |thrust = {{convert|286|kN}} |SI = 247 sec |burntime = 27 seconds |fuel = Solid |type = Stage |stageno = Third |name = Antares 1A |engines = 1 X-254 |thrust = {{convert|60|kN}} |SI = 256 sec |burntime = 39 seconds |fuel = Solid |type = Stage |stageno = Fourth |name = Altair 1A |engines = 1 X-248A |thrust = {{convert|14|kN}} |SI = 255 sec |burntime = 40 seconds |fuel = Solid |type = Stage |stageno = Fifth |name = NOTS-17 |engines = 1 solid |thrust = |burntime = |fuel = Solid }} 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 NOTS-17 upper stage. The Scout X-1A used an Algol 1C first stage, instead of the earlier Algol 1B 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 {{convert|214|km}}, and was successful. Following this, the Scout X-1A was replaced by the Scout X-2. References{{refbegin}}
2 : 1962 in spaceflight|Scout (rocket family) |
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