Expander cycle
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- A Performance Analysis of a Rocket Based Combined Cycle (RBCC) Propulsion System for Single-Stage-To-Orbit Vehicle Applications
- Component Tests of a LOX/Methane Full-Expander Cycle Rocket Engine: Electrically Actuated Valve
- Upper Stage Liquid Propellant Rocket Engine: a Case Analysis
- Component Tests of a LOX/Methane Full-Expander Cycle Rocket Engine: Injector and Regeneratively Cooled Combustion Chamber
- Parametric Study of Dual-Expander Aerospike Nozzle Upper-Stage Rocket Engine
- Design of a Centrifugal Pump for an Expander Cycle Rocket Engine
- Expander Demonstrator
- Methane Dual Expander Aerospike Nozzle Rocket Engine Michael D
- Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine
- High Performance Lox Hydrogen Upper Stage with Pistonless Pump
- (12) United States Patent (10) Patent No.: US 8,572,948 B1 Pinera (45) Date of Patent: Nov
- Design of a Dual-Expander Aerospike Nozzle Rocket
- High Speed Propulsion Cycles
- Design of an Oxygen Turbopump for a Dual Expander Cycle Rocket Engine
- Space Exploration & Space Colonization Handbook
- 69674 3 En Bookfrontmatter 1..61
- A Single-Stage Reusable Launch Vehicle Concept Abbos Yunusov A