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NASA Sp8089 Injector Designs
Historical liquid rocket engine injector design data from NASA SP-8089 Table I (pp.3-6). Each record is one operational engine/injector assembly covering 22 engines from Redstone (1950s) through SSME (1970s). Fields include combustion efficiency (eta_c), thrust, chamber pressure, injector diameter, element type, element counts, orifice diameters, materials, and combustion stabilization devices.
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Redstone A71 rowJupiter1 rowThor MB31 rowAtlas MA5 Booster1 rowAtlas MA5 Sustainer1 rowTitan I Booster1 rowTitan I STAGE21 rowSaturn Ib H11 rowSaturn Ic F11 rowAgena LR811 rowLance Booster1 rowLance Sustainer1 rowTitan II Booster1 rowTitan II STAGE21 rowTranstage AJ101 rowTitan III Booster1 rowApollo Sps1 rowApollo Lem Descent1 rowApollo Lem Ascent1 rowSaturn J21 rowCentaur RL101 rowSsme1 row