RM-89 Blue Scout I

RM-89 Blue Scout I

Blue Scout D6 ahead of the second HETS launch
Function	Sounding rocket
Manufacturer	Vought
Country of origin	United States
Size
Height	21.65 metres (71.0 ft)
Diameter	1.02 metres (3 ft 4 in)
Mass	16,738 kilograms (36,901 lb)
Stages	Three
Associated rockets
Family	Scout
Derivatives	RM-90 Blue Scout II
Launch history
Status	Retired
Launch sites	Canaveral LC-18B
Total launches	3
Successes	1
Failures	2
First flight	1961-01-07
Last flight	1962-04-12
First stage – Algol 1B
Engines	1 solid
Thrust	471 kilonewtons (106,000 lbf)
Specific impulse	236 sec
Burn time	40 seconds
Fuel	Solid
Second stage – Castor 1A
Engines	1 solid
Thrust	286 kilonewtons (64,000 lbf)
Specific impulse	247 sec
Burn time	27 seconds
Fuel	Solid
Third stage – Antares 1A
Engines	1 X-254
Thrust	60 kilonewtons (13,000 lbf)
Specific impulse	256 sec
Burn time	39 seconds
Fuel	Solid

The RM-89 Blue Scout I was an American sounding rocket which was flown three times between January 1961 and April 1962. It was used for two HETS test flights, and a flight to investigate atmospheric re-entry. It was a member of the Scout family of rockets.

The Blue Scout I was a three-stage rocket derived from the Scout X-1. All three launches occurred from Launch Complex 18B at the Cape Canaveral Air Force Station. The first two launches were conducted on 7 January and 9 May 1961 respectively. They both carried HETS A1 plasma research experiments on suborbital trajectories. The third launch was conducted on 12 April 1962, with a payload that was intended to investigate atmospheric reentry.

The first launch was successful, however recovery of the payload failed. Both other launches failed due to problems with the Blue Scout.

The Blue Scout II was a four-stage derivative of the Blue Scout I. It was flown three times in 1961, twice with HETS payloads, and once with the Mercury-Scout 1 satellite.