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| Figure | 8.BOMARCandTalosRamjet-AssistedMiss1les…8 |
|---|---|
| Figure | 9.PositronSSRVFlightProfile••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••••10 |
| Figure | 10.Artist’sRenditionofaFour-EnginePositronSSRV…11 |
| Figure | 11.Solid-CorePositronRocketEngineWithaHot-BleedConfiguration•••••12 |
| Figure | 12.FluidSystems…•…•…•… 11•••11•••••••••••••••••111•••••••••••••••••15 |
| Figure | 13.ModifiedSangerPhotonRocketConcept…17 |
| Figure | 14.ClosedBraytonCycleUsingPositronAnnihilation…18 |
| Figure | 15.Conceptual110WattPositronClosedCycleGeneratorBasedonthe |
| NASAGlennResearchCenterStirlingRadioisotopeGenerator(SRG)••18 | |
| Figure | 16.MarsTrajectories(X-CoordinatesDefinedinDirectionofAries)…20 |
| Figure | 17.SpacecraftsUsingPositronEngines…21 |
| Figure | 18.ProposedUndulator-BasedPositronSourcefortheInternational |
| Linear Collider …22 | |
| Figure | 19..PenningTrap…24 |
| Figure | 20.A PositronForl11SPs…25 |
| Figure | 21.ComputerSimulationofPsAtoms…26 |
| Figure | 22.TEMofSilicaAerogel•••••••••••••••••••••••••••••••••.••••.••••••.••••••.••••••••••••••••••••••26 |
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| Vehicle Component Structure Thermal Protection Propulsion (4 engines) Electronics TOTALDRYMASS 15%Margin+Unused Propellants Payload BURNOUTMASS TOTAL PROPELLANT GLOW Mass 25,700 kg 12,300 kg 14,900 kg 7,600 kg 60,500 kg 11,400 kg 11,340 kg (24,948 Ibs) 83,240 kg 176,000 kg 259,240 k 590,328 Ibs |
|---|
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| MissionMode Turbojet - Launch Ramjet 10%margin(turbojet mode upon landing, inclination changes, etc.) TOTAL MassOfe! 2,5mg 76.5mg 7.9rng 86.9mg |
|---|
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| Source | $/JOULE annihilation Now 333* | |
|---|---|---|
| 2011/19 0.410.004** |
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