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Launch Systems | Space Systems | Mission Engineering


In the present budget environment, there is a strong need to dramatically drive down the cost of space missions. There is the perception that SmallSats are inherently much lower cost than more traditional larger satellites and can play a central role in reducing overall space mission cost, but this effect has been difficult to quantify in the past. Without quantifiable evidence of their value, SmallSats are under-utilized as a method for reducing space mission cost. The purpose of this study is to quantify the relationship between cost and performance for space systems, by creating a Performance-Based Cost Model (PBCM). Today, most acquisition performance analyses focus on cost overruns, or how much the system costs relative to what it is expected to cost. Instead, PBCM allows us to focus on more important questions, such as, how much performance we can achieve for a given cost, or what the cost is for a given level of performance. In this report, we present the relationship between cost vs. orbit altitude for a fixed resolution and coverage requirement, cost vs. resolution, and cost vs. coverage. Traditional cost models for space systems are typically weight-based, primarily because mass allocation is determined early in mission design and has historically correlated well with actual hardware cost. To provide the underlying cost data for this study, we apply three cost models widely used throughout the aerospace cost modeling community: the Unmanned Space Vehicle Cost Model (USCM8), the Aerospace Corp. Small Satellite Cost Model (SSCM), and the NASA Instrument Cost Model (NICM).
Our first application of the PBCM is for Earth observing systems. Past Earth observation systems have used traditional space technology to achieve the best possible performance, but have been very expensive. In addition, low-cost, responsive dedicated launch has not been available for SmallSats. Space system mass is proportional to the cube of the linear dimensions—equivalent to saying that most spacecraft have about the same density. This means that by flying at lower altitudes, satellites can reduce their payload size and therefore the entire mass of the satellite, thus reducing the cost of the system dramatically. We conclude that for an Earth observation system, an increase in performance, reduction in cost, or both, is possible by using multiple SmallSats at lower altitudes when compared to traditional systems. Specifically,

  • By using modern microelectronics and light-weight materials such as composite structures, future SmallSats observation systems, operating at a lower altitude than traditional systems, have the potential for:
    • Comparable or better performance (resolution and coverage)
    • Much lower overall mission cost (by a factor of 2 to 10)
    • Comparable or better performance (resolution and coverage
    • Much lower overall mission cost (by a factor of 2 to 10)
    • Lower risk (both implementation and operations)
    • Shorter schedules
  • Relevant secondary advantage for the low-altitude SmallSats include:
    • Lower up-front development cost
    • More sustainable business model
    • More flexible and resilient
    • More responsive to both new technologies and changing needs
    • Mitigates the problem of orbital debris

The principal demerits of the approach are the lack of low-cost launch vehicles, the need for a new way of doing business, and changing the way we think about the use of space assets. This paper provides the basis for this assessment, estimates for the level of cost reduction, and reports on additional results since the 2013 Reinventing Space Conference.

Download “Quantifying the Cost Reduction Potential for Earth Observation Satellites”

Shao, A., E.A. Koltz and J.R. Wertz. 2014. AIAA Space and Astronautics Forum and Exposition (SPACE 2014), San Diego, CA. August 4–7, 2014.