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Launch Systems | Space Systems | Mission Engineering

Development of the Scorpius LOX/Kerosene Engine Family

Abstract: Microcosm and Sierra Engineering have been developing a series of low-cost pressure fed LOX/kerosene engines to power the Scorpius® family of launch vehicles. This paper focuses on the design, fabrication and testing of a 20K lbf O-F-O triplet injector with...

Development of the Scorpius® LOX/Kerosene Engine Family

Abstract: Microcosm and Sierra Engineering have been developing a series of low-cost pressure fed LOX/kerosene engines to power the Scorpius® family of launch vehicles. This paper focuses on the design, fabrication and testing of a 20K lbf O-F-O triplet injector with...

Rapid Interplanetary Round Trips at Moderate Energy

Abstract: We define a new class of “rapid round trip” interplanetary missions for which the principal characteristic is a total mission duration that is 1 or more years shorter than the traditional round trip using Hohmann transfers. Round trip missions using Hohmann...

Responsive Access to Space—The Scorpius® Low-Cost Launch System

Abstract: “Responsive space” has substantial benefit in terms of both flexibility to meet real-time needs and assured space access. However, creating responsive space requires a new paradigm for space launch systems, launch operations, and the space systems...

Responsive Launch Vehicle Cost Model

Abstract: This paper presents a launch vehicle cost model designed specifically to estimate the additional economic cost of two related system properties that have substantial military utility — responsiveness and surge capability. In addition, the model can be used...

Self-Configuring Network for Launch Vehicle and Satellite Avionics

Abstract: Under an Air Force Phase II SBIR contract, Microcosm is developing a self-configuring avionics network, scheduled for test on a sounding rocket in late 2003 or early 2004. This system is extendable to spacecraft avionics and housekeeping functions, enabling...

Interplanetary Round Trip Mission Design

Abstract: This paper defines the basic constraints for interplanetary round trip travel or, equivalently, for round trip travel from and to a natural or artificial satellite, such as round trips from the International Space Station to another satellite and back. While...