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Methodology for Determining the Optimal Mass Ratio of Fuel Charges for an Aft Gas Generator and a Rocket Engine from the Perspective of Achieving Maximum Range
| Authors: Vetrov V.V., Shilin P.D. | Published: 10.07.2026 |
| Published in issue: #7(796)/2026 | |
| Category: Aviation, Rocket and Technology | Chapter: Aircraft Development, Design and Manufacture | |
| Keywords: aft gas generator, solid-propellant rocket motor, equivalent specific impulse, base drag, combined propulsion system, maximum flight range |
On the Influence of Physical Limits on the Range of a Hypersonic Flight Vehicle
| Authors: Presnyakov S.V., Usachev V.A., Koryanov V.V., Kudryavtseva N.V. | Published: 26.07.2018 |
| Published in issue: #7(700)/2018 | |
| Category: Aviation, Rocket and Technology | Chapter: Aerodynamics and Heat Transfer Processes in Aircraft | |
| Keywords: ramjet engine, combustion chamber pressure, aerodynamic heating, weight analysis, maximum flight range |
