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NAA 75-110 A-7

The NAA 75-110 A-7 was the final Redstone engine variant in the NAA 75-110 series, developed by Rocketdyne from the XLR43-NA-1 lineage. NASA identifies the A-7 as the final A-series design at 78,000 lbf (about 347 kN) for 117 seconds in the standard Redstone configuration; Jupiter-C and Juno I used modified Redstone stages with installation-specific fuel and burn-duration context. The engine powered Redstone-derived Jupiter-C/Juno I and Mercury-Redstone vehicles.

NAA 75-110 A-7
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Identity

Aliases
Rocketdyne NAA 75-110 A-7Rocketdyne A-775-110 A-7A-7
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
NAA 75-110 A-7
Status
retired

Details

Description
The NAA 75-110 A-7 was the final Redstone engine variant in the NAA 75-110 series, developed by Rocketdyne from the XLR43-NA-1 lineage. NASA identifies the A-7 as the final A-series design at 78,000 lbf (about 347 kN) for 117 seconds in the standard Redstone configuration; Jupiter-C and Juno I used modified Redstone stages with installation-specific fuel and burn-duration context. The engine powered Redstone-derived Jupiter-C/Juno I and Mercury-Redstone vehicles.
Developers
Manufacturers
Propellants
ethyl alcoholliquid oxygen
Rocket Specs
Burn Time S
117
Chamber Count
1
Sea Level Thrust Kn
347

Links

Assets & Meta

Creation Time
July 29, 2026 at 11:08:58 UTC
Updated Time
August 22, 2026 at 06:12:05 UTC

Other

Sources