Delta·McDonnell Douglas
Delta III 8930
retired
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Specifications
- Status
- retired
- Height
- 35 m
- Diameter
- 4 m
- Mass
- 301,000 kg
- Stages
- 2
- Thrust
- 4,889 kN
- Payload to LEO
- 8,290 kg
- Payload to GTO
- 3,810 kg
- First flight
- 1998-08-26
- Total launches
- 3
- Success / Fail
- 1 / 2
The Delta III rocket was an expendable launch vehicle made by Boeing. The first Delta III launch was on August 26, 1998.
Propulsion
First stage
RS-27A1,054 kN
RP-1 / LOX · gas-generator
RocketdyneIsp 302s (vac)since 1990
Second stage
AJ-1043 kN
NTO / Aerozine-50 · pressure-fed
Aerojet RocketdyneIsp 319s (vac)since 1962
Payloads it launched
2 loaded