Juno II (1958-1961)
First Flight: 1958
Last Flight: 1961
Stages: 4
Total Mass: 55.11 tons
Payload Mass: 41 kg to LEO
Diameter: 2.67 m
Length: 24 m
First Stage
Type: Core
Arrangement: 1 x Rocketdyne S-3D
Thrust (kN): 667
Propellant: LOX/RP-1
ISP: 248 s
ISP (sea level):
Burn Time: 182 s
Gross Mass: 54.43 tons
Second Stage
Type: Core
Arrangement: 11 x MGM-29 Sergeant solid
Thrust (kN): 73
Propellant: polysulfide-aluminum and ammonium perchlorate
ISP: 214 s
ISP (sea level):
Burn Time: 6 s
Gross Mass: 0.462 tons
Empty Mass: 0.231 tons
Third Stage
Type: Core
Arrangement: 3 x MGM-29 Sergeant solid
Thrust (kN): 20
Propellant: polysulfide-aluminum and ammonium perchlorate
ISP: 214 s
ISP (sea level):
Burn Time: 6 s
Gross Mass: 0.126 tons
Empty Mass: 0.063 tons
Fourth Stage
Type: Core
Arrangement: 1 x MGM-29 Sergeant solid
Thrust (kN): 7
Propellant: polysulfide-aluminum and ammonium perchlorate
ISP: 214 s
ISP (sea level):
Burn Time: 6 s
Gross Mass: 0.042 tons
Empty Mass: 0.021 tons
I think tthis iss amonng thhe mosst immportant informaton forr mе.
Annd i’m hapy stuudying yoour article. Buut ԝant too obbservation onn ffew commo tɦings, Thhe
wweb site stype iss ideal, tthe articfles iss reallky grat : Ɗ.
Goodd job, cheers
Alsoo visitt mmy webpage – penthouse malaysia