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Delta · McDonnell Douglas

Delta 2914

retired
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Specifications

Status
retired
Height
35 m
Diameter
2.44 m
Mass
130,000 kg
Stages
4
Payload to LEO
724 kg
First flight
1974-04-13
Total launches
30
Success / Fail
28 / 2

The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.

Payloads it launched · 31

WESTAR 3
GEO
SCATHA
GEO
NATO 3C
GEO
ISEE-3 (ICE)
Heliocentric
GEOS-2
GEO
GOES 3
GEO
YURI (BS)
GEO
IUE
GEO
SAKURA (CS)
GEO
METEOSAT-1
GEO
ISEE-2
HEO
ISEE-1
HEO
HIMAWARI-1 (GMS-1)
GEO
GOES 2
GEO
GEOS-1
GEO
PALAPA 2
GEO
NATO 3B
GEO
MARISAT 2
GEO
PALAPA 1
GEO
MARISAT 3
GEO
NATO 3A
GEO
MARISAT 1
GEO
CTS
GEO
GOES 1 (SMS-C)
GEO