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RM-90 Blue Scout II

Spacecraft and Launch Vehicles

The RM-90 Blue Scout II was an American sounding rocket and expendable launch system in the Scout family, flown three times during 1961. It was a military version of the NASA-operated Scout X-1, with adjustments to the payload fairings, engine nozzles and fins. The four-stage vehicle was 21.65 metres long with a fin span of 2.84 metres and used four solid-propellant stages, Algol 1B, Castor 2, Antares 1A and Altair 1A, to put a 30 kilogram payload into a 300 kilometre orbit. Two flights in March and April 1961 carried HETS plasma experiments on suborbital paths. The third, on 1 November 1961, was meant to orbit the Mercury-Scout 1 satellite for NASA but went out of control and was destroyed by the range safety officer 43 seconds after liftoff. It and the Blue Scout I were later replaced by Blue Scout Junior.

Facts
Year
1961 1
Propulsion
Solid propellant 1
Engine Class
Rocket 1
Status
Retired from service 1
Comparison
Body Style
Sounding rocket 1
Body Style
Launch vehicle 1
Connections

Derived From

Scout X-1, Vehicles
Source RM-90 Blue Scout II (Wikipedia)

Exemplifies

Source RM-90 Blue Scout II (Wikipedia)
In the Other Atlases

Originated In

Also in Geography Atlas: where this subject originated.

Source RM-90 Blue Scout II (Wikipedia)Lead, body style
Quote, Lead, body style
was an American sounding rocket and expendable launch system
Sources
1. RM-90 Blue Scout II (Wikipedia)
  • Lead
    which was flown three times during 1961
  • Lead, body style
    was an American sounding rocket and expendable launch system
  • Lead, launch system
    was an American sounding rocket and expendable launch system
  • Stages, rocket
    Stage 1: Algol 1B, solid propellant
  • Lead, replacement
    This rocket and RM-89 Blue Scout I were replaced by Blue Scout Junior.
  • Derived From: Scout X-1, Lead, military version
    Blue Scout II was a military version of the NASA-operated Scout X-1
View the Source
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