Delta 0100-series (0300 and 0900)

Country of Origin: United States
Manufacturer: McDonnell Douglas

Height:
Diameter: 2.44 m core, 0.79 m boosters
Payload to LEO: 1300 kg (747-818 kg to SSO)
Total Mass:

Launch Sites: Vandenberg
First Flight: July 23, 1972
Last Flight: November 6, 1973
Total Launches: 5
Successful Launches: 4

Delta 0300

Stage	Diameter	Propellant	Engine	Time	Thrust (Vac.)	ISP (SL/Vac.)
Boosters	0.79 m	Solid	3 x Castor 2	37 s	3 x 259 kN	? / 262 s
1 (Thor)	2.44 m	RP-1 / LOX	MB-3-III		866.7 kN	253 / 290 s
2 (Delta)	1.4 m	UDMH / RFNA	AJ-10-118F	335 s	41.4 kN	? / 306 s

Delta 0900

Stage	Diameter	Propellant	Engine	Time	Thrust (Vac.)	ISP (SL/Vac.)
Boosters	0.79 m	Solid	9 x Castor 2	37 s	9 x 259 kN	? / 262 s
1 (Thor)	2.44 m	RP-1 / LOX	MB-3-III		866.7 kN	253 / 290 s
2 (Delta)	1.4 m	UDMH / RFNA	AJ-10-118F	335 s	41.4 kN	? / 306 s

Links: