space spiral reliability schedule - usra-houstonmars pathfinder (1996, $265m) deployed the first...

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1. Problem NASA will not achieve the Discovery and New Frontiers cadence recommended by the last decadal survey 2 Planetary science is stuck in the “Space Spiral(Fig. 1) 3 Competed PI-led missions were established to save money but they experience an average of 35% cost growth, similar to missions led by NASA centers 4 Questioning the status quo in pursuit of lowering planetary mission costs Elizabeth Frank First Mode, Seattle, WA, USA (elizabeth@firstmode.com) NOTE: Risk ≠ Reliability! Reliability = system dependability Risk = chance of undesireable event × consequences (e.g., technical, cost, schedule, politicial, etc.) A low-cost mission that is not high-reliability can be lower in risk than a Flagship mission because the consequences are less impactful 3. Take Action! Participate in smallsat opportunities such as SIMPLEX Charge your assumptions about how missions “should” be done (section 2C) Gain historical perspective by reading about FBC (start here: bit.ly/2TEeDNx) Collaborate with New Space companies, which rely on lean management and innovation for survival Advocate for rebalancing NASA’s risk portfolio with a new planetary smallsat program via: Assessment/Analysis Group meetings and recommendations Activities related to the next Planetary Science Decadal Survey KEY POINT: To more cost-effectively explore the solar system, the planetary science community must question its assumptions and culture regarding missions. “The largest obstacle to low-cost innovation is the belief that it cannot be done.” 1 2. Solution A. Lean Management After the Viking launches in 1978, no planetary missions launched for 11 years due to schedule and cost overruns 5 (Fig. 2) 1990s NASA used “Faster, Better, Cheaper” (FBC) practices, including lean management, to break the 1980s Space Spiral but abandoned FBC after 4 mission failures in 1999 1 Failure overshadows FBC’s successes, which included 5 low-cost planetary science missions (Fig. 3): NEAR Shoemaker (1996, $212M*) landed on S-type asteroid Eros Mars Pathfinder (1996, $265M) deployed the first rover on Mars, Sojourner Lunar Prospector (1998, $63M) confirmed the presence of water ice on the Moon Mars Global Surveyor (1998, $219M) returned high-res imagery and topography of Mars Stardust (1999, $200M) returned material from the coma of comet Wild 2 FBC missions produced more publications (a proxy for science return) per dollar than traditionally managed missions 6 *Costs are provided from the missions’ websites in real year USD and include launch. For reference, $212M in 1996 USD is the equivalent of $341M in 2019 USD. The current Discovery cost cap is $450M excluding launch. How the Space Spiral works Cost: labor drives mission costs, not hardware; longer schedules lead to higher costs Reliability: complex, expensive missions are risky, demanding high reliability Schedule: high reliability is ensured through extra testing, which lengthens development and lessens mission cadence B. Small Spacecraft Smallsats’ low mass (<180 kg dry) and correspondingly low cost permit in-space testing of new technologies and architectures MarCO’s success in November 2018 proved that CubeSats can work in deep space (Fig. 4) NASA’s Earth Sciences Division created the Venture class of low-cost missions ($100-200M) as recommended by the 2007 Earth Science Decadal Survey. 6 CYGNSS has been monitoring extreme weather since 2016 using 8 25-kg spacecraft C. Cultural Change “There’s a paradox at work here that creates a downward spiral. Launching fewer spacecraft means scientists want to pile every instrument they can onto whatever’s going to fly. That increases the weight, which increases the cost of the spacecraft and the launcher. Fewer spacecraft also means we can’t take any risk with the ones we launch, so we have to have redundancy, which increases weight and cost, and we can risk flying new technology, so we don’t end up producing cutting edge technology.” -NASA Administrator Daniel Goldin, 1992 The quote is from 1992 but still applies today. Here’s what you can do to effect cultural change: Resist the urge to turn every spacecraft into a Swiss Army Knife of instrumentation Accept that cost reduction is possible and achievable 4 Understand that low cost does not equate to low reliability 4 Embrace the elegance of simple missions with focused objectives and few instruments Be open to novel mission architectures that leverage unique smallsat capabilities Scan this QR code for a PDF of this poster: References 1 McCurdy H. (2003) Faster, Better, Cheaper, JHU Press 2 NRC (2018) V&V: A Midterm Review, Nat. Acad. Press 3 Wertz J. et al. (2011) Space Mission Engineering, Microcosm Press 4 Yoshida J. et al. (2013) 2013 IEEE Conference 5 Siddiqi A. (2018) Beyond Earth, NASA report SP-2018-4041 6 Dillon R. and Madsen P (2015) IEEE Trans. Eng. Mgmt. 62, No. 2 7 NRC (2007) Earth Science Applications from Space, Nat. Acad. Press Fig 4. An engineer with the two MarCO CubeSats, one with solar panels unfurled (NASA/JPL). Fig. 1. The “Space Spiral” feedback loop 3 increased costs higher reliability demanded longer schedules/ decreased mission cadence Fig 2. (above) Masses of U.S. deep space spacecraft launched through 2016. Note the dearth of missions between 1978 and 1989 as well as the low-mass, high-cadence FBC period in the 1990s. Data from [5]. Fig. 3. (right) Achievements from planetary Faster, Better, Cheaper era missions. (A) NEAR’s last image from Eros (NASA/APL). (B) Comet particles in aerogel returned by Stardust (Smithsonian). (C) Neutron Spectrometer data confirming Lunar Prospector’s discovery of water ice (Los Alamos). (D) High-res Mars Global Surveyor image (MSSS/ NASA/JPL). (E) Pathfinder panorama of landing site and Sojourner deployment (NASA/JPL). A B D C E

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Page 1: Space Spiral Reliability Schedule - USRA-HoustonMars Pathfinder (1996, $265M) deployed the first rover on Mars, Sojourner Lunar Prospector (1998, $63M) confirmed the presence of water

1. Problem• NASA will not achieve the Discovery and New Frontiers

cadence recommended by the last decadal survey2

• Planetary science is stuck in the “Space Spiral” (Fig. 1)3

• Competed PI-led missions were established to save money but they experience an average of 35% cost growth, similar to missions led by NASA centers4

Questioning the status quo in pursuit of lowering planetary mission costsElizabeth Frank

First Mode, Seattle, WA, USA ([email protected])

NOTE: Risk ≠ Reliability!

Reliability = system dependability

Risk = chance of undesireable event × consequences (e.g., technical, cost, schedule, politicial, etc.)

A low-cost mission that is not high-reliability can be lower in risk than a Flagship mission because the

consequences are less impactful

3. Take Action!• Participate in smallsat opportunities such as SIMPLEX

• Charge your assumptions about how missions “should” be done (section 2C)

• Gain historical perspective by reading about FBC (start here: bit.ly/2TEeDNx)

• Collaborate with New Space companies, which rely on lean management and innovation for survival

• Advocate for rebalancing NASA’s risk portfolio with a new planetary smallsat program via:

• Assessment/Analysis Group meetings and recommendations

• Activities related to the next Planetary Science Decadal Survey

KEY POINT: To more cost-effectively explore the solar system, the planetary science community must question its assumptions and culture regarding missions. “The largest obstacle to low-cost innovation is the belief that it cannot be done.”1

2. SolutionA. Lean Management

• After the Viking launches in 1978, no planetary missions launched for 11 years due to schedule and cost overruns5 (Fig. 2)

• 1990s NASA used “Faster, Better, Cheaper” (FBC) practices, including lean management, to break the 1980s Space Spiral but abandoned FBC after 4 mission failures in 19991

• Failure overshadows FBC’s successes, which included 5 low-cost planetary science missions (Fig. 3): NEAR Shoemaker (1996, $212M*) landed on S-type asteroid Eros

Mars Pathfinder (1996, $265M) deployed the first rover on Mars, Sojourner

Lunar Prospector (1998, $63M) confirmed the presence of water ice on the Moon

Mars Global Surveyor (1998, $219M) returned high-res imagery and topography of Mars

Stardust (1999, $200M) returned material from the coma of comet Wild 2

• FBC missions produced more publications (a proxy for science return) per dollar than traditionally managed missions6

*Costs are provided from the missions’ websites in real year USD and include launch. For reference, $212M in 1996 USD is the equivalent of $341M in 2019 USD. The current Discovery cost cap is $450M excluding launch.

How the Space Spiral works

Cost: labor drives mission costs, not hardware; longer schedules lead to higher costs

Reliability: complex, expensive missions are risky, demanding high reliability

Schedule: high reliability is ensured through extra testing, which lengthens development and lessens

mission cadence

B. Small Spacecraft

• Smallsats’ low mass (<180 kg dry) and correspondingly low cost permit in-space testing of new technologies and architectures

• MarCO’s success in November 2018 proved that CubeSats can work in deep space (Fig. 4)

• NASA’s Earth Sciences Division created the Venture class of low-cost missions ($100-200M) as recommended by the 2007 Earth Science Decadal Survey.6 CYGNSS has been monitoring extreme weather since 2016 using 8 25-kg spacecraft

C. Cultural Change

“There’s a paradox at work here that creates a downward spiral. Launching fewer spacecraft means scientists want to pile every instrument they can onto whatever’s going to fly. That

increases the weight, which increases the cost of the spacecraft and the launcher.

Fewer spacecraft also means we can’t take any risk with the ones we launch, so we have to have redundancy, which increases weight and cost, and we can risk flying new technology, so

we don’t end up producing cutting edge technology.”-NASA Administrator Daniel Goldin, 1992

The quote is from 1992 but still applies today. Here’s what you can do to effect cultural change:

• Resist the urge to turn every spacecraft into a Swiss Army Knife of instrumentation

• Accept that cost reduction is possible and achievable4

• Understand that low cost does not equate to low reliability4

• Embrace the elegance of simple missions with focused objectives and few instruments

• Be open to novel mission architectures that leverage unique smallsat capabilities

Scan this QR code for a PDF of this poster:

References1McCurdy H. (2003) Faster, Better, Cheaper, JHU Press2NRC (2018) V&V: A Midterm Review, Nat. Acad. Press3Wertz J. et al. (2011) Space Mission Engineering, Microcosm Press4Yoshida J. et al. (2013) 2013 IEEE Conference5Siddiqi A. (2018) Beyond Earth, NASA report SP-2018-40416Dillon R. and Madsen P (2015) IEEE Trans. Eng. Mgmt. 62, No. 2 7NRC (2007) Earth Science Applications from Space, Nat. Acad. Press

Fig 4. An engineer with the two MarCO CubeSats, one with solar panels unfurled (NASA/JPL).

Fig. 1. The “Space Spiral” feedback loop3

increasedcosts

higherreliability

demanded

longer schedules/decreased mission cadence

Fig 2. (above) Masses of U.S. deep space spacecraft launched through 2016. Note the dearth of missions between 1978 and 1989 as well as the low-mass, high-cadence FBC period in the 1990s. Data from [5].

Fig. 3. (right) Achievements from planetary Faster, Better, Cheaper era missions. (A) NEAR’s last image from Eros (NASA/APL). (B) Comet particles in aerogel returned by Stardust (Smithsonian). (C) Neutron Spectrometer data confirming Lunar Prospector’s discovery of water ice (Los Alamos). (D) High-res Mars Global Surveyor image (MSSS/NASA/JPL). (E) Pathfinder panorama of landing site and Sojourner deployment (NASA/JPL).

A B

D

C

E