Scout X-1A Explained

Manufacturer:Vought
Country-Origin:United States
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
Si:236 sec
Burntime:40 seconds
Type:Stage
Stageno:Second
Si:247 sec
Burntime:27 seconds
Type:Stage
Stageno:Third
Si:256 sec
Burntime:39 seconds
Type:Stage
Stageno:Fourth
Si:255 sec
Burntime:40 seconds
Type:Stage
Stageno:Fifth

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, and was successful. Following this, the Scout X-1A was replaced by the Scout X-2.

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