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Cornell Space Systems Design Studio

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Science. In-orbit test to raise TRL. Technology demo for a sponsor. Engineering research ... Expanded launch opportunities accelerate science and technology ... – PowerPoint PPT presentation

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Title: Cornell Space Systems Design Studio


1
CornellSpace Systems Design Studio
  • Near-Term Mission
    Concepts Funding Models for Small Spacecraft

Mason Peck Assistant Professor Mechanical and
Aerospace Engineering 607-255-4023
CUSat 1 2, Summer 2008
2
Why bother with a low-cost, quick-response launch
vehicle?
  • Overview
  • Mine is not the VC perspective
  • Spacecraft capabilities in the pico- to
    nano-satellite class
  • Categories of small-satellite missions of current
    interest
  • Example mission concepts
  • Prospective funding
  • What if there were a low-cost, quick-response
    launch vehicle?

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
3
Pico- and Nanosatellite Capabilities
  • Picosat 0.1 - 10 kg
  • Cubesat
  • AMSAT Deck of Cards
  • Aerospace Corp / DARPA picosat
  • Nanosat 10-100 kg
  • University nanosatellites (UNP)
  • AMSAT OSCARs
  • DARPA F6 modules (?)

10x10x10 cm
Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
50x50x60 cm
4
Pico- and Nanosatellite Capabilities
  • For now
  • Picosats
  • Cubesat lt 4W, Some lt 0.1W
  • lt 10 cm aperture
  • lt9600 Baud
  • GPS, coarse attitude control
  • Nanosats
  • lt120W
  • lt40 cm aperture
  • S Band
  • GPS, fine attitude control
  • Propulsion
  • Cooperative formation

Protoflight Cubesat with GPS for ionnospheric
science (ICE Cubesat)
Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
Pulsed-Plasma Thruster Test
5
Pico- and Nanosatellite Capabilities
  • Soon
  • Picosats
  • Micropropulsion
  • Nanosats
  • High agility

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
6
Categories of Missions
  • Research
  • Science
  • In-orbit test to raise TRL
  • Technology demo for a sponsor
  • Engineering research
  • DoD
  • Responsive Space (ORS)
  • Networked communications (Space Based Group /
    DARPA F6)
  • Space Situational Awareness
  • Intelligence, Surveillance, Reconnaissance
  • Education

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
7
Example Mission Objectives
  • Research

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
8
Example Mission Objectives
  • DoD

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
9
Example Mission Objectives
  • Education

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
10
Prospective Funding
  • DoD (ORS et al)
  • Other Government
  • DARPA
  • NRO
  • NASA? AFOSR? NSF?
  • Industry (academic partnerships for low-cost,
    one-off demos)
  • IRD, BP
  • Commercial startups
  • Microgravity enterprises
  • Throw water at the moon

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
11
What if?
  • Very small spacecraft
  • Exploit scaling for new flight dynamics gt new
    CONOPs

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
Image courtesy of Bob Sauls / Popular Science
12
What if?
  • Snowball effects
  • Volume ltgt cost grows the industry
  • Educational opportunities graduate more
    spacecraft engineers and grow the industry
  • Expanded launch opportunities accelerate science
    and technology
  • Increased space access and lower-cost components
    encourages manned space

Agenda Pico to nano capabilities Categories of
missions Mission concepts Prospective
funding What if
13
Toward a Standard Nanosatellite Orbit
  • Imagine a MIL STD orbit for nanosats, e.g.
    circular, 500 km, equatorial
  • Future NLVs might be built to accommodate this
    standard
  • Why? From the LV perspective
  • Vastly simpler design and IT well-understood
    customer needs
  • Common capabilities for components such as
    guidance hardware and separation mechanisms (
    sep requirements)
  • If you build it they will come--like the Cubesat
    standard, but for mission design and operations.
  • Why? From the Nanosat payload perspective
  • Most nanosats care little about orbit science,
    tech demos, short lifetime, etc. so, pick the
    most convenient one
  • Use LEO to ensure drag sweeps the orbit clean of
    debris
  • A small number of equatorial ground stations can
    provide considerable TC coverage. These ground
    stations should use specific frequencies (e.g.
    amateur radio).
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