Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
Details
- OL Work ID
- OL11152496W
Subjects
Body-wing configurationsAerodynamic characteristicsWind tunnel testsLongitudinal stabilitySubsonic speedAerodynamic stabilityAngle of attackSingle stage to orbit vehiclesSideslipAerodynamic forcesLateral stabilityControl surfacesTransonic speedMach numberSpacecraft stability