Delta 3910/PAM
In-activeMcDonnell Douglas (MDC)
Nov. 15, 1980
Description
The Delta 3000 series was an American expendable launch system which was used to conduct 38 orbital launches between 1975 and 1989. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.
Specifications
-
Stages
4 -
Length
35.0 m -
Diameter
2.44 m -
Fairing Diameter
2.44 m -
Launch Mass
191.0 T -
Thrust
3188.0 kN
Family
-
Name
Delta 3910/PAM -
Family
― -
Variant
3910/PAM -
Alias
― -
Full Name
Delta 3910/PAM
Payload Capacity
-
Launch Cost
― -
Low Earth Orbit
1087.0 kg -
Geostationary Transfer
Orbit
― -
Direct Geostationary
― -
Sun-Synchronous Capacity
―
McDonnell Douglas
Commercial
None
MDCNone
Delta 3910/PAM | Westar 5
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June 9, 1982, 12:24 a.m.
Delta 3910/PAM | Insat 1A
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April 10, 1982, 6:47 a.m.
Delta 3910/PAM | Westar 4
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Feb. 26, 1982, 12:04 a.m.
Delta 3910/PAM | Satcom 4
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Jan. 16, 1982, 1:55 a.m.
Delta 3910/PAM | Satcom 3R
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Nov. 20, 1981, 1:37 a.m.
Delta 3910/PAM | SBS 2
McDonnell Douglas | United States of AmericaCape Canaveral SFS, FL, USA
Sept. 24, 1981, 11:09 p.m.
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