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Aerojet AJ10-101
The pressure-fed hypergolic propulsion system used on the historical Thor-Able second stage.
Identity
Domains
spaceflight
Identity Level
variant
Kind
liquid-rocket-engine
Name
Aerojet AJ10-101
Status
historical
Details
Description
The pressure-fed hypergolic propulsion system used on the historical Thor-Able second stage.
Family
Family
Links
Official Url
https://ntrs.nasa.gov/citations/19980230605
Assets & Meta
Creation Time
July 29, 2026 at 08:10:53 UTC
Updated Time
July 29, 2026 at 08:13:50 UTC
Other
Sources
Accessed Date
2026-07-29
Note
Supports the legacy vehicle installation and the narrow canonical identity used for migration.
Publisher
Official vehicle or program source
Title
Thor-Able IV Launch Vehicle official vehicle reference
Url
https://ntrs.nasa.gov/api/citations/19880016045/downloads/19880016045.pdf
Accessed Date
2026-07-29
Note
Supports the legacy vehicle installation and the narrow canonical identity used for migration.
Publisher
Official vehicle or program source
Title
Thor-Able I Lunar Launch Vehicle official vehicle reference
Url
https://ntrs.nasa.gov/citations/19980230605
Accessed Date
2026-07-29
Note
Supports the legacy vehicle installation and the narrow canonical identity used for migration.
Publisher
Official vehicle or program source
Title
Atlas-Able Lunar Launch Vehicle official vehicle reference
Url
https://science.nasa.gov/wp-content/uploads/2023/09/DSC_monograph24.pdf
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