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MB-3-3
MB-1/MB-3 -
Credit: Mark Wade. 6,405 bytes. 127 x 235 pixels.
Designer
: Rocketdyne.
Used on stages
:
Delta Thor LT
,
Delta Thor TA
,
H-1-1
.
Used on launch vehicles
:
Delta 100
,
Delta D
,
Delta E
,
Delta G
,
Delta J
,
Delta L
,
Delta M
,
Delta N
,
H-1
,
LT Thor Agena D
,
TA Thor Agena B
,
TA Thor Agena D
. Propellants:
Lox/Kerosene
Thrust(vac)
: 88,380 kgf.
Thrust(vac)
: 866.70 kN.
Isp
: 290 sec.
Isp (sea level)
: 253 sec.
Burn time
: 270 sec.
Mass Engine
: 723 kg.
Diameter
: 2.4 m.
Length
: 1.7 m.
Chambers
: 1.
Chamber Pressure
: 39.00 bar.
Area Ratio
: 8.00.
Thrust to Weight Ratio
: 122.24.
Country
: USA.
Status
: Out of Production.
First Flight
: 1963.
Last Flight
: 1992.
Flown
: 172.
Comments
: License built in Japan for H-1.
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Last update 12 March 2001.
Definitions of Technical Terms
.
Contact
Mark Wade
with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site.
.
© Mark Wade, 2001 .
