Ares V RFP: Looking for a Few Good Requirements

On Jan. 5, NASA issued a request for proposal for Phase I concept definition and requirements development for the Ares V heavy lift rocket. The Ares V is a key transportation system for exploration beyond low Earth orbit, as well as NASA’s primary vessel for safe, reliable delivery of large-scale hardware to space. It is a primary component of the Constellation Program to help carry human explorers back to the moon, then onward to Mars and other destinations in the solar system.

Ares V offers unprecedented payload capabilities — 40 percent more payload to Trans Lunar Injection (TLI) by itself than the Saturn V was designed to deliver.  In combination with Ares I, it can deliver nearly 60% more to TLI than Saturn V.  The Ares V increased payload and volume capability will make it the largest launch vehicle ever built as well as a national asset with potential users outside NASA. The astronomy, planetary science and Earth science communities already have shown interest in Ares V.

For such a large endeavor, the Ares team at Marshall has strategically solicited the help of other NASA programs, NASA centers, experts with experience going back to the Saturn and Apollo development, as well as industry expertise to create the best design possible for the nation’s next space craft to the moon and beyond. This desire for input from various areas of expertise is captured in the recent Ares V Request for proposal (RFP).

What’s in the RFP?
The Ares V Phase I solicitation includes five separate work packages available for bid. The packages include evaluation of specific Ares V elements including the payload shroud that will protect the Altair lunar lander during launch, the Earth Departure Stage, the core stage, and avionics and software. The products for these packages include assessing risks and opportunities for the point of departure (POD) architecture, trade studies and analysis, assessment of NASA requirements and a final report. The fifth work package includes a first stage concept for an upgraded solid rocket fueled booster. It will focus on exploring booster options and abilities to increase performance and operability.

Proposals are due Feb. 17. Contracts are slated to be awarded in March or April 2009. The period of performance for each contract is 18 months with two, one-year options. Multiple awards per element could be awarded.

NASA-led assessments, analysis and trade studies coupled with industry study packages will feed into the final POD architecture and element definition for Phase I. This work will enable the Ares V team to move to element prime contracts for Phase II in the 2012 timeframe.
 
What Does Phase I Include?

Phase I will focus on defining system level requirements, validating that they can be accomplished with maximum utility in regard to cost, reliability, operability and performance and reducing risk for design, development, test and evaluation (DDT&E).

In Phase I, NASA is engaging industry to assess our designs, identify risks and opportunities, and develop trade studies and analyses. This is to ensure we clearly define our concept of operations, requirements, interfaces, and design concepts for Ares V prior to prime contractor procurement activities.

Phase I will include contractor support to NASA design efforts through the Ares V Systems Requirements Review (SRR) in June 2011 and the System Definition Review (SDR) slated for spring 2012.

Small Steps to a Great Adventure


If the greatest adventures begin with small steps, the Constellation Program took giant strides in 2008 and has more planned for 2009. Here is an excerpt from the year’s-end note, dated December 2008, Constellation Program Manager Jeff Hanley sent to his team.


All, as I type this I’m coming to the end of nearly a full week in our nation’s capitol, and here at the end of our third year as a team I owe you an update from 50,000 feet (sorry, 15 km). I think it’s important that our entire team have this context, so that we can together take on the challenges that 2009 will surely bring.

First, as I review the events of 2008, and the progress that we together have made across this agency team, I am truly proud of what you have accomplished — and you should be too. Today we have projects and hardware and software in nearly every phase of the lifecycle, from pre-formulation of our lunar surface strategy and the international partnerships that are already beginning to form, to formal formulation of the Ares V and Altair requirements, to completion of the program definition phase for Ares I, Orion, and their sister projects, to the testing of engine components and fabrication of flight test hardware for Pad Abort 1 and Ares I-X.

The program has built considerable momentum in the past 12 months and indeed over the last three years since we stood up as a team. We’ve done it for a fraction of the cost in people and resources compared to Apollo, shuttle and station through this phase. We’ve done it while the same supporting institutions execute our other two human spaceflight programs. We’ve done it with focus and resolve to transition shuttle workforce and assets to the new program in the smartest way possible. We’ve done it — done it all — with the Moon as our goal. “Design for lunar” has guided our every move, our every decision, within the bounds of what we can fiscally afford through these lean years until shuttle is retired.

I know you all have seen the public discourse regarding Ares and Orion and shuttle, and understandably such discourse can temper our resolve to push forward — if we let it. But, let’s review the bidding. First, we should remind ourselves, as we saw in intimate detail at last summer’s Lunar Capability Concept Review (arguably the finest such review the team has yet executed), that the Ares I/Ares V/Orion/Altair transportation system is highly integrated and keenly designed to open the lunar frontier to us in the years to come. Our driving requirements of going anywhere on the Moon, staying twice as long as Apollo in a sortie mode, sending twice as many crew members, and enabling their return at any time, must remain at the forefront of any consideration to alter the nation’s exploration launch architecture. I assure each of you that we are doing all we can to communicate this key aspect of our baseline plan — it is about much more than launching Orion to LEO (Low Earth Orbit).

The shuttle team, as you know, has performed a study of projected cost and decision points for extending the life of shuttle. I have not seen the report in its final form so I won’t comment on the interim version. But I will say — will reassure you — that Constellation’s needs, interests, and requirements were central to their deliberations, and we were partnered closely with the study team to provide the Constellation implications of any extension. It was a good effort and I am quite satisfied that any impacts to Constellation are well accounted for.

Somewhat in tandem, in October we kicked off our own special study led by Ralph Roe out of NESC (NASA Engineering and Safety Center) to look at options to accelerate Constellation to allow the first human flight to occur prior to our March 2015 commitment date. All of the deputy managers of our program and project offices participated, along with a substantial number of experienced contributors from outside the program. It took our most recent baseline plan — including budgets, schedules, technical content, risks and threats, and assessed achievability of three different acceleration cases to improve upon the March of 2015 commitment date, assuming of course that resources were added to do so. Ralph briefed the draft report to leadership at HQ (NASA Headquarters), and while it is still being finalized, the findings are not new — the upshot being, if you want to accelerate Ares I and Orion then significant new money must be added to the Constellation budget in FY09 and FY10. This is the same answer that we provided more than a year ago when asked what it would take to keep our September 2013 baseline with an adequate level of confidence.

And no wonder – if you look at a “traditional” funding profile for an aerospace program and compare it to the Constellation budget profile, the deficit in these early years is obvious. What it compels us to do, therefore, is defer some key work to later that would buy down considerable risk — flight and ground tests, manufacturing demos, test articles to investigate structural margins, engineering development units, buys of long lead parts, etc. This is where we are at today with our internal target of September 2014, compounded by very lean reserves in these same two years to deal with surprises.

We’re at where we’re at. In the weeks ahead we will proceed assuming no new money will be forthcoming to accelerate and we will instead move forward to adjust our plan to meet our March 2015 commitment. If a decision comes forward to accelerate by the April timeframe, an earlier date is still possible, but that gets less and less likely with each passing month.

Again, none of this should be a surprise — though some will feign shock and accuse us of overselling. But we have been very careful these three years to avoid that. We have consistently pointed out that our internal ‘work to’ dates were aggressive with this fiscal profile and what additional funding it would take to increase our confidence and ability to execute. These same realities have been reinforced by those who independently review us. Throughout we have applied common government and industry practices and methods for how projects and programs are funded and managed. We kept the option open to enable a more aggressive date as long as we reasonably could before last summer’s re-baselining. Two years of continuing resolutions haven’t helped, but we’ve worked around them to the best of our ability to keep moving forward.

Look at all you’ve accomplished in spite of that!!

All this is offered as context to further amplify what an amazing result — in spite of it all — that 2008 has produced. Constellation is not a paper program anymore. It is a full-fledged assault on the frontier, and if we keep the mission at the forefront of our sights then we can persevere. As the year draws to a close, we enjoy broad support in Congress, we have a vision that we’ve not only embraced but have strategically over the last three years codified in an exploration architecture with a broad range of capability to allow us to unlock first cis-lunar space and then the inner solar system in the years to come… and who knows what other missions these new tools might be employed for?

In the coming year, let’s continue to make history — one milestone at a time — as we celebrate those whose shoulders we stand upon more than a generation ago.

Ares: America's Rocket for Future Space Missions

 

How did NASA select the Ares family of rockets as America’s new space transportation system?

Since the 1980’s, NASA has evaluated thousands of studies relating to space transportation. It has been said we could “pave” the way to the moon with all the studies that have been conducted. These studies looked at thousands of combinations and variations of how to send humans beyond low Earth orbit, back to the moon and on to Mars. 

NASA looked at a wide variety of launch concepts — from the Evolved Expendable Launch Vehicle (Atlas V, Delta IV), Space Shuttle (including Shuttle C, Direct type approaches and other solid and liquid rocket booster propelled systems) combinations, foreign systems and clean sheet designs.

The Exploration Systems Architecture Study (ESAS) was chartered in the spring of 2005 to recommend a fundamental architecture for supporting International Space Station, Lunar and Mars transportation.

Using data from previous and ongoing studies (several hundred vehicles), and consisting of a team of knowledgeable experts from inside and outside NASA, this study compared many launch and staging options for safety, effectiveness, performance, flexibility, risk and affordability.

ESAS concluded that NASA should adopt and pursue a Shuttle-derived architecture as the next-generation launch system, using a smaller vehicle for crew missions and a dedicated, heavy-lift launcher for cargo missions. This approach was selected due to several significant advantages, particularly safety, reliability and cost.

NASA continued to refine its launch recommendations post-ESAS. Since early 2006 NASA has made the following major modifications to the initial designs.

Upgraded from the shuttle’s four-segment reusable solid rocket booster design (RSRB) to a five-segment RSRB design — forming a common basis for Ares I and V Eliminated the space shuttle main engine (SSME) in favor of a newly designed J-2X engine for the Ares I upper stage. The Ares V upgraded from a five-segment RSRB with expendable SSME Core to a derivative of the Ares I 1st stage with a six-engine RS-68 Core and the J-2X engine for the earth departure stage (EDS).

Developing the new J-2X engine for both the Ares I upper stage and the Ares V Earth departure stage solves several potential problems including starting the SSME at altitude and the major expense of using it for the first stage engine. For additional cost savings Ares will use the expendable RS-68 engine which is “off the shelf” technology that meets both Department of Defense and NASA needs.

These combined changes represent a projected savings of over $5 billion in life cycle costs below the initial ESAS recommendations.

The shuttle heritage design offers years of proven flight concepts with a very strong technical and safety foundation for next-generation vehicle. Since ESAS, NASA has continued to assess options — over 1,700 to date. After a thorough analysis of all the exploration architecture requirements, other solutions were ultimately determined to be less safe, less reliable, and more costly than Ares I and Ares V.

Throughout the selection process for its launch vehicles, NASA has been thorough, transparent, subject to regular independent reviews, open to alternative ideas, and has made all of its decisions based on hard data.

Ares is a solid foundation for America’s future in space.

Practicing for the Moon

Here’s a picture of NASA’s Lunar Electric Rover getting ready to practice docking with some lunar habitat mockups. Test engineers at the Johnson Space Center spent the day recently seeing how the rover docked with different habitat configurations. The one you see in the picture hasn’t been tested yet, but is called the Toroidal Habitat Mockup. It’s basically a giant plywood mockup of an inflatable donut-shaped habitat that is giving the teams ideas of what will work best on the moon.