Transforming NASA Technology Innovation with a new Business Model for Partnership
Topic: This paper proposes a method of streamlining and expediting technology transfer from NASA to the private sector by developing contracted Technology Maturation and Transfer Centers (TMTCs). These TMTCs would document, advance, and transfer NASA-developed technologies to outside parties.
Authors: Jason Hundley
Presented/Published: Civil Space Symposium 2013
Sponsoring Customer/Organization: AIAA
Engine-Out Capabilities Assessment of Heavy Lift Launch Vehicles
Topic: Derived top-level approach to engine-out philosophy for a heavy lift launch vehicle based on an historical assessment of launch vehicle capabilities. Methodology not intended to present best path forward, but instead provides three parameters for assessment of a particular vehicle: Reliability (Loss of Mission & Loss of Crew), vehicle performance and cost.
Authors: Jon Holladay, Keithe Baggett, Chad Thrasher, K. Scott Bellamy, Stuart Feldman
Presented/Published: 2012 IEEE Aerospace Conference, Big Sky, MT, March 2012
Sponsoring Customer/Organization: MSFC
Space Launch System Mission Flexibility Assessment
Topic: Discussion of the alternative mission scenarios that were examined during post- Requirements Analysis Cycle (RAC) activities.
Author(s): Timothy Monk, Jon Holladay, Bryan Hampton, Terry Sanders
Presented at/published in: GLEX 2012, Washington, D.C., May 2012
Sponsoring Customer/Organization: MSFC
An Evaluation of the Global Exploration Roadmap Using an Established Framework Based on Historical Exploration Roadmaps, Initiatives, and Systems
Topic: Description of the Roadmap Evaluation Framework developed by ZPFC for evaluation and comparison of space roadmaps.
Author(s): Erica Hampton, Keithe Baggett, Karin Feldman
Presented at/published in: GLEX 2012, Washington, DC, May 2012
Sponsoring Customer/Organization: JSC
Complex Decision-Making Applications for the NASA Space Launch System
Topic: Description of the decision-making framework ZPFC developed for the SLS Program management team.
Author(s): Garry Lyles, Tim Flores, Jason Hundley, Timothy Monk, Stuart Feldman
Presented at/published in: 2012 IEEE Aerospace Conference, Big Sky, MT, March 2012
Sponsoring Customer/Organization: MSFC
Engine-Out Capabilities Assessment of Heavy Lift Launch Vehicles
Topic: Derived top-level approach to engine-out philosophy for a heavy-lift launch vehicle based on an historical assessment of launch vehicle capabilities. The methodology was not intended to present a best path forward, but instead provide three parameters for assessing a particular vehicle: reliability (loss of mission & loss of crew), vehicle performance and cost.
Authors: Jon Holladay, Keithe Baggett, Chad Thrasher, K. Scott Bellamy, Stuart Feldman
Presented/Published: 2012 IEEE Aerospace Conference, Big Sky, MT, March 2012
Sponsoring Customer/Organization: MSFC
Next Generation Heavy-Lift Launch Vehicle: Large Diameter, Hydrocarbon-Fueled Concepts
Topic: A discussion of the Space Launch System (SLS) RAC Team 2 concept trade space, including all branches examined and description of the preferred option.
Author(s): Jon Holladay, Timothy Monk, Charles Adams, Ricky Campbell
Presented at/published in: 2012 IEEE Aerospace Conference, Big Sky, MT, March 2012
Sponsoring Customer/Organization: MSFC
Two Space Exploration Roadmaps (v3 – ISDC)
Topic: How Propulsion Technology Shaped Beyond-Low-Earth-Orbit Exploration Roadmaps.
Authors: S Feldman, E Hampton, K Baggett, J Hundley, K Feldman
Presented at: 2011 International Space Development Conference (ISDC 2011) May 18-22, 2011
Sponsoring Customer: JSC
Abstract submitted: March 2011
IEEE: Earth Departure Stage Technology Requirements for a Mars DRM
Topic: This paper introduces technologies that need to be developed to undertake the human mission to Mars. Mars DRA5.0 has summarized these requirements at a high level, leveraging decades of NASA and other independent studies. The Ares V Vehicle Integration and EDS teams have investigated what these technologies actually mean to the heavy-lift vehicle and its associated elements. Overall, in-space cryogenic propellant transfer, automated rendezvous & docking, and low-to-zero-boil-off technologies have a place in future human expansion across the inner solar system.
Author(s): Timothy Monk, Jon Holladay, Keithe Baggett, Stuart Feldman
Presented at: 2011 IEEE Aerospace Conference; Big Sky Montana; March 5-12
Sponsoring Customer/Organization: MSFC
Two Space Exploration Roadmaps (v2 – AIAA)
Topic: How Technology Shapes Our Plans for Space Exploration: A Case Study of Two Eras.
Authors: S Feldman, E Hampton, K Baggett, J Hundley, K Feldman
Presented at: AIAA Space 2011
Sponsoring Customer: JSC
Abstract submitted: January 24, 2011
Executive Summary of Ares V: LCCR through PA-C3
Topic: Ares V trade studies, analyses performed, and extensibility options captured in an all-inclusive summarizing document. Appendices (e.g. EDS, Docking Adapter, etc.) may be generated later and coupled with this Executive Summary for a more detailed story.
Author(s): Keithe Baggett, Stuart Feldman, Jon Holladay
Presented at/published in: Technical Memorandum
Sponsoring Customer/Organization: MSFC
IEEE: Heavy Lift Contributions to a Human Mission to Mars
Topic: A consolidated version of the Mars TM. Assessment of the ability of the Ares V vehicle (POD PA-C3D) to support the reference approach for the crewed Mars mission as defined in the Mars Design Reference Architecture (DRA 5.0) via the NTP and chemical options.
Author(s): Jon Holladay, John Jaap, Robin Pinson, Steve Creech, Rick Ryan, Timothy Monk, Keithe Baggett, Mike Runager, Ian Dux, Kurt Hack, Jason Hopkins, Chad Brown and Tedd Manning
Presented at: 2011 IEEE Aerospace Conference; Big Sky Montana; March 5-12
Sponsoring Customer/Organization: MSFC
Analysis of Shroud Options in Support of the Human Exploration of Mars
Topic: Discussion of the launch vehicle shroud technology considered for the Ares V vehicle when applied to the Mars mission – including the dual-use shroud and Mars entry analysis performed to support the Mars Design Reference Architecture 5.0 (DRA 5.0).
Author(s): Stuart Feldman, Stan Borowski, Walt Engelund, Jason Hundley, Timothy Monk, Michelle Munk
Presented at: 2010 IEEE Aerospace Conference, Big Sky, Montana; March 2011
Sponsoring Customer/Organization: MSFC
Mars TM: Ares V Utilization in Support of a Human Mission to Mars
Topic: Assessment of the ability of the Ares V vehicle (POD PA-C3D) to support the reference approach for the crewed Mars mission as defined in the Mars Design Reference Architecture (DRA 5.0) via Nuclear Thermal Propulsion (NTP) and chemical options.
Author(s): Jon Holladay, John Jaap, Robin Pinson, Steve Creech, Rick Ryan, Timothy Monk, Keithe Baggett, Mike Runager, Ian Dux, Kurt Hack, Jason Hopkins, Chad Brown and Tedd Manning
Published in: NASA Technical Memorandum 2010-216450
Sponsoring Customer/Organization: MSFC
Propellant Mass Fraction Calculation Methodology for Launch Vehicles and Application to Ares Vehicles
Topic: Discussion of various methods for calculating propellant mass fraction (pmf) and how mission requirements can influence that particular metric of launch vehicle structural efficiency.
Author(s): Barney Holt and Timothy Monk
Presented at: Space 2009, Pasadena, CA; September 2009
Sponsoring Customer: MSFC
100-Year Starship Organization Construct Recommendation: Private Foundation 5 Jul 2011
Topic: Discussion of societal and economic forces that should be considered when structuring a 100-year starship program, focusing primarily on types of organizations that could successfully accomplish an ultra-long-term program. Paper focuses on main recommendation of a Private Foundation development model.
Author: Timothy Monk, Stuart Feldman, Jason Hundley
To be presented at: 100 Year Starship Symposium, Orlando, FL, Sept. 30th-Oct. 2nd
Sponsoring Customer: TBD
Abstract Submitted: 7.6.2011
100 Year Starship Non-FTL Mission Sequence 5 Jul 2011
Topic: How to progressively expand outward to interstellar space with non-faster-than-light (FTL) technologies.
Author: Stuart Feldman, Bryan Hampton, Timothy Monk
To be presented at: 100 Year Starship Symposium, Orlando, FL, Sept. 30th-Oct. 2nd
Sponsoring Customer: TBD
Abstract Submitted: 7.6.2011
Two Space Exploration Roadmaps
Topic: A Discussion of Two Space Exploration Roadmaps: Comparing and Contrasting Dynamic Points in the Space Industry During the 1960s and the 1980s.
Authors: S Feldman, E Hampton, K Baggett, J Hundley
To be presented at: NASA History 1961/1981
Sponsoring Customer: JSC
Engine-Out Capabilities Assessment of Heavy Lift Launch Vehicles_03062012.pdf
12 Nov, 10.5 MB
An Evaluation of the Global Exploration Roadmap Using an Established Framework Based on Historical Exploration Roadmaps, Initiatives, and Systems
Topic: Description of the Roadmap Evaluation Framework developed by ZPFC for evaluation and comparison of space roadmaps
Author(s): Erica Hampton, Keithe Baggett, Karin Feldman
To be presented at/published in: GLEX 2012, Washington, D.C., May 2012
Sponsoring Customer/Organization: JSC
An Evaluation of the Global Exploration Roadmap Using an Established Framework Based on Historical Exploration Roadmaps, Initiatives, and Systems.pdf
16 May, 2.1 MB
Space Launch System Mission Flexibility Assessment
Topic: Discussion of the alternative mission scenarios that were examined during post-RAC activities
Author(s): Timothy Monk, Jon Holladay, Bryan Hampton, Terry Sanders
To be presented at/published in: GLEX 2012, Washington, D.C., May 2012
Sponsoring Customer/Organization: MSFC
GLEX(3)-SLS Mission Flexibility Assessment.pdf
2 May, 1.1 MB
Next Generation Heavy-Lift Launch Vehicle: Large Diameter, Hydrocarbon-Fueled Concepts 1
Topic: A discussion of the Space Launch System (SLS) Requirements Analysis Cycle (RAC) Team 2 concept trade space – including all branches examined and description of the preferred option
Author(s): Jon Holladay, Timothy Monk, Charles Adams, Ricky Campbell
To be presented at/published in: 2012 IEEE Aerospace Conference, Big Sky, MT, March 2012
Sponsoring Customer/Organization: MSFC
NGHLLV.pdf
1 Nov 2011, 1.5 MB
Two Space Exploration Roadmaps (v2 – AIAA)
Topic: How Technology Shapes Our Plans for Space Exploration: A Case Study of Two Eras
Authors: S Feldman, E Hampton, K Baggett, J Hundley, K Feldman
To be presented at: AIAA Space 2011
Sponsoring Customer: JSC
Abstract submitted: January 24, 2011
AIAA Space 2011 Abstract ZPFC Space Exploration Roadmap Technologies Submitted.pdf
24 Jan 2011, 62.7 KB
aiaa roadmap presentation.pptx
11 Oct 2011, 9.7 MB
Two Space Exploration Roadmaps (v3 – ISDC)
Topic: How Propulsion Technology Shaped Beyond-Low-Earth-Orbit Exploration Roadmaps
Authors: S Feldman, E Hampton, K Baggett, J Hundley, K Feldman
To be presented at: 2011 International Space Development Conference (ISDC 2011) May 18-22, 2011
Sponsoring Customer: JSC
Abstract submitted: March 2011
20110519 ZPFC Roadmaps Propulsion Technologies.docx
13 Jun 2011, 6.1 MB
20110519 ZPFC Roadmaps Propulsion Technologies.pptx
13 Jun 2011, 11.5 MB
Executive Summary of Ares V: LCCR through PA-C3
Topic: Ares V trade studies, analyses performed and extensibility options captured in an all-inclusive summarizing document. Appendices (e.g. EDS, Docking Adaptor, etc) may be generated later and coupled with this Executive Summary for a more detailed story.
Author(s): Keithe Baggett, Stuart Feldman, Jon Holladay
To be presented at/published in: Technical Memorandum
Sponsoring Customer/Organization: MSFC
Executive Summary of Ares V- Lunar Capabilities Concept Review Through Phase A-Cycle 3.pdf
28 Feb 2011, 17.6 MB
Mars TM: Ares V Utilization in Support of a Human Mission to Mars
Topic: Assessment of the ability of the Ares V vehicle (POD PA-C3D) to support the reference approach for the crewed Mars mission as defined in the Mars Design Reference Architecture (DRA 5.0) via the NTP and chemical options.
Author(s): Jon Holladay, John Jaap, Robin Pinson, Steve Creech, Rick Ryan, Timothy Monk, Keithe Baggett, Mike Runager, Ian Dux, Kurt Hack, Jason Hopkins, Chad Brown and Tedd Manning
Published in: NASA Technical Memorandum 2010-216450
Sponsoring Customer/Organization: MSFC
NASA_Mars DRM TM.pdf
25 Jan 2011, 19.4 MB
IEEE: Earth Departure Stage Technology Requirements for a Mars DRM
Topic: This paper introduces technologies that need to be developed in order to undertake the human mission to Mars. Mars DRA5.0 has summarized these requirements at a high-level leveraging decades of NASA and other independent studies. The Ares V Vehicle Integration and EDS teams have investigated what these technologies actually mean to the heavy-lift vehicle and its associated elements. Overall, in-space cryogenic propellant transfer, automated rendezvous & docking, and low-to-zero boiloff technologies have a place in future human expansion across the inner solar system.
Author(s): Timothy Monk, Jon Holladay, Keithe Baggett, Stuart Feldman
Presented at: 2011 IEEE Aerospace Conference; Big Sky Montana; March 5-12
Sponsoring Customer/Organization: MSFC
EDS Technology Requirements for the Mars DRM.pdf
25 Jan 2011, 1.2 MB
IEEE: Heavy Lift Contributions to a Human Mission to Mars
Topic: A consolidated version of the Mars TM. Assessment of the ability of the Ares V vehicle (POD PA-C3D) to support the reference approach for the crewed Mars mission as defined in the Mars Design Reference Architecture (DRA 5.0) via the NTP and chemical options.
Author(s): Jon Holladay, John Jaap, Robin Pinson, Steve Creech, Rick Ryan, Timothy Monk, Keithe Baggett, Mike Runager, Ian Dux, Kurt Hack, Jason Hopkins, Chad Brown and Tedd Manning
Presented at: 2011 IEEE Aerospace Conference; Big Sky Montana; March 5-12
Sponsoring Customer/Organization: MSFC
Heavy Lift Contributions to a Human Mission to Mars.pdf
25 Jan 2011, 7.9 MB
Analysis of Shroud Options in Support of the Human Exploration of Mars
Topic: Discussion of the launch vehicle shroud technology considered for the Ares V vehicle when applied to the Mars mission – including the dual use shroud and Mars entry analysis performed in support of Mars Design Reference Architecture 5.0 (DRA 5.0).
Author(s): Stuart Feldman, Stan Borowski, Walt Engelund, Jason Hundley, Timothy Monk, Michelle Munk
Presented at: 2010 IEEE Aerospace Conference, Big Sky, Montana; March 2011
Sponsoring Customer/Organization: MSFC
IEEEshrouds122109.pdf
19 May 2011, 10.6 MB
Propellant Mass Fraction Calculation Methodology for Launch Vehicles and Application to Ares Vehicles
Topic: Discussion of various methods for calculation propellant mass fraction (pmf) and how mission requirements can influence that particular launch vehicle structural efficiency metric.
Author(s): Barney Holt and Timothy Monk
Presented at: Space 2009, Pasadena, CA; September 2009
Sponsoring Customer: MSFC
PMF Calculation Methodology_MonkHolt_5.pdf
19 May 2011, 2 MB
Space 2009 Poster email.jpg
