STAR 37FMV
STAR 37FMV is a titanium-case solid upper-stage motor with an electromechanically actuated flexseal nozzle. Minotaur V offers it for three-axis-stabilized fifth-stage operation. The TE-M-1139 catalogue configuration has a 62.7 s burn and 293.7 s effective vacuum specific impulse.
Identity
- Aliases
- STAR-37FMVSTAR37FMV
- Domains
- spaceflight
- Identity Level
- variant
- Kind
- solid-rocket-motor
- Name
- STAR 37FMV
- Status
- unknown
Details
- Description
- STAR 37FMV is a titanium-case solid upper-stage motor with an electromechanically actuated flexseal nozzle. Minotaur V offers it for three-axis-stabilized fifth-stage operation. The TE-M-1139 catalogue configuration has a 62.7 s burn and 293.7 s effective vacuum specific impulse.
- Family
- Length
- …
- Manufacturers
- Propellants
- TP-H-3340 solid propellant
- Rocket Specs
- Burn Time
- …
- Vacuum Specific Impulse
- …
Links
Assets & Meta
- Creation Time
- October 29, 2026 at 15:57:53 UTC
- Updated Time
- October 29, 2026 at 15:57:53 UTC
Other
- Diameter
- …
- Sources
- Accessed Date
- 2026-10-29
- Note
- 2013 manufacturer fact sheet hosted by NASA: separate spin-stabilized STAR 37FM and three-axis STAR 37FMV fifth-stage alternatives.
- Publisher
- Orbital Sciences / NASA
- Title
- Minotaur V High Energy Space Launch Vehicle fact sheet
- Accessed Date
- 2026-10-29
- Note
- Exact model table, printed page 96: dimensions converted from inches, burn time distinct from action time and effective Isp distinct from propellant Isp. Current production lifecycle is not established by the historical catalogue.
- Publisher
- Northrop Grumman
- Title
- Propulsion Products Catalog — STAR 37FMV