"Asteroid Retrieval
Feasibility Study" (.pdf), 2 April 2012, Prepared for the Keck
Institute for Space Studies, California Institute of Technology, Jet
Propulsion Laboratory, Pasadena, CA.
Planetary Resources
website
- "Planetary Resources is establishing a new paradigm for resource
discovery and utilization that will bring the solar system into
humanity’s sphere of influence."
February 2, 2012
"NASA Space Technology Roadmaps
and Priorities, Restoring NASA’s Technological Edge and Paving the Way
for a New Era in Space", Steering Committee for NASA Technology
Roadmaps, Aeronautics and Space Engineering Board, Division on
Engineering and Physical Sciences, National Research Council.
[Paper
.pdf]
"Additional Comments: The development timeline for launch propulsion
technologies will be critically dependent on the overall strategy
and architecture chosen for exploration and the funding available.
Of particular relevance is launch economics,
particularly with regards to the launch rate and the mass of
missions being launched. Additionally, there are technologies
included in other roadmaps, especially TA02 (In-Space Propulsion)
and TA04 (Robotics, Tele-Robotics, and Autonomous Systems) that open
the trade space to other architecture options, such as fuel depots
requiring on-orbit propellant transfer technologies. For example,
one may be able to disaggregate some large space missions to be
launched by larger numbers of smaller, lower cost launch vehicles.
These technologies may allow more dramatic reductions in
launch costs than specific launch technologies themselves."
August
10, 2011
"Pros, Cons, and
Alternatives to Weight Based Cost Estimating" (.pdf format), presented at the
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July
31 - August 3, 2011, San Diego California, by C.R. Joyner II, Pratt &
Whitney Rocketdyne, West Palm Beach, Florida,
Jonathan R. Laurie, Pratt & and D.J.H.
Levack, Pratt & Whitney Rocketdyne, Canoga
Park, California, and E. Zapata, NASA Kennedy
Space Center, Florida.
Above - from the paper -
"Figure 8.0 Historic rocket engine cost breakdown"
August 3, 2011
"High-Payoff
Space Transportation Design Approach with a Technology Integration
Strategy" (.pdf format), presented at the 47th
AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 31 -
August 3, 2011, San Diego California, by C. M. McCleskey and R. E. Rhodes, NASA Kennedy Space
Center, Florida, T. T. Chen, NASA Marshall Space Flight Center,
Huntsville Alabama, and J. W. Robinson, Propellant Supply
Technology Inc., California.
"This paper describes a
general approach for creating architectural concepts that are highly
efficient, operable, and supportable, in turn achieving affordable,
repeatable, and sustainable space transportation. The paper focuses on
the following: (1) vehicle architectural concept (including important
strategies for greater reusability), (2) vehicle element propulsion
system packaging, including integrated main and auxiliary propulsion
systems, (3) vehicle element functional integration, (4) ground
element functional integration, (5) simplified and automated
electrical power and avionics integration, and (6) ground and flight
testing before production commitments. We also provide four essential
technologies that enable the high-payoff design approach: (a)
parallel-tank propellant storage, such as concentric-nested tanks, for
more efficient space vehicle design and operation, (b) high-thrust,
LO2-rich, LO2-cooled first-stage earth-to-orbit main engine, (c)
nontoxic, day-of-launch-loaded propellants for upper stages and
in-space propulsion, and (d) electric controls for propulsion."
Above - from the paper -
"Figure 1. Closed-compartment entry for personnel requiring design and
operations effort, resulting lost time and productivity."
"As shown in Figure 5.1,
the Project Budget showed that peak funding would occur in the same
year as the Project PDR and that Project costs would go down by 16% in
FY 2009 and 58% in FY 2011. Historically, the cost profiles of
projects continue to increase after PDR. Based on the technical status
of the Project, the prior deferral of spacecraft development, and the
complexity of the integration and testing phase, this was a highly
suspect budget profile."
"Launch Vehicle Propulsion
Life Cycle Cost Lessons Learned" (.pdf), Presented
at the AIAA Joint Propulsion Conference July
26-28, 2010, Nashville TN by - Edgar Zapata and
Russel E. Rhodes, NASA Kennedy Space Center,
Florida & John W. Robinson, The Boeing
Company, Huntington Beach, California
Sustainability: Competitiveness,
Economics, Business and Acquisition Models
A
launch abort system (LAS) can address many
shortcomings in the reliability of launch vehicle
systems by rapidly removing a crew from harms
way. It is worth emphasizing that a launch abort
system does not address inherent hardware
reliability, it's quality. From an operational
standpoint a launch abort system adds complexity
and reduces operability. There is more work to
prepare for launch, rather than less, all else
being equal. A launch abort system merely reacts
to the reliability (or lack thereof) of the
launch vehicle hardware.
A
launch abort systems primary purpose is to improve
the metric of loss of crew, or simply put - to
improve crew safety during a portion of the mission,
during a portion of the climb to orbit. These video's
show alternate launch abort system designs recently
tested by NASA.
DATA: "Developing
a Robust, Adaptable NASA Human Space Flight
Strategy Factoring Budgetary and Technological
Uncertainty" or "The Primer" to NASA &
Contractor Costs (October 10, 2009,
Post-Augustine Committee)
"Shuttle Shortfalls and
Lessons Learned for the Sustainment of Human
Space Exploration", Presented at the 45th
AIAA/ASME/SAE/ASEE Joint Propulsion Conference,
AIAA 2009-5346, 2-5 August 2009, Denver, Colorado by - Edgar Zapata,
NASA, Kennedy Space Center, Florida & Daniel
J. H. Levack, Pratt & Whitney Rocketdyne,
Canoga Park, California & Russel E. Rhodes,
NASA, Kennedy Space Center, Florida & John W.
Robinson, The Boeing Company, Huntington Beach,
California
"The Joint Confidence Level
Paradox, A History of Denial", by Glenn
Butts, NASA Kennedy Space Center, and Kent
Litton, SAIC/Craig Technologies [Download 3MB .pdf].
"The authors provide Historical
Evaluation of Cost and Schedule Estimating
Performance During NASA's Tenure as an Agency -
Following which they introduce an optimum Hybrid
model for more accurately calculating Cost and
Schedule estimates in NASA's Complex systems
engineering environment."
Sustainability
2008
The Global
Exploration Strategy, A framework for Coordination: Download report here or
here.
"Sustainable
space exploration is a challenge that no one
nation can do on its own. This is why fourteen
space agencies have developed The Global
Exploration Strategy: The Framework for
Coordination, which presents a vision for robotic
and human space exploration, focusing on
destinations within the solar system
where
we may one day live and work. It
elaborates an action plan to share the strategies
and efforts of individual nations so that all can
achieve their exploration goals more effectively
and safely."
In
alphabetical order: ASI (Italy), BNSC (United
Kingdom), CNES (France), CNSA (China), CSA
(Canada), CSIRO (Australia), DLR (Germany), ESA
(European Space Agency), ISRO (India), JAXA
(Japan), KARI (Republic of Korea), NASA (United
States of America), NSAU (Ukraine), Roscosmos
(Russia). "Space Agencies" refers to
government organizations responsible for space
activities.
The
following data relates especially well to Space
Transportation Systems Affordability, Responsiveness,
Reliability and Safety. The quality of hardware and
software systems, as manifest in launch vehicle failure
rates, beckons for improvement. The visible failure
rates, during flight, and the less visible failures
during ground processing, causing unplanned work, are
inter-connected quality and technology issues for the
aero-industry.