- \n
- Augustine Forum Section<\/li>\n
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- Click here to Join L2<\/li>\n<\/ul>\n
Despite what can only be described as politically-driven armwaving from the Aerospace Safety Advisory Panel (ASAP), very few people of power are taking any stock in their recommendations, notably to continue to focus on the Program Of Record (POR) based around Ares I, and their continued distain at the evaluations to extend the shuttle program past 2010.<\/p>\n
While Ares I is suffering from death throes, NASA managers have openly noted on documentation that they are evaluating commercial crew launch options for transporting astronauts to the International Space Station (ISS) in four to five years time. Current favorite for providing this role is the Atlas V-Heavy.<\/p>\n
ASAP\u2019s negativity surrounding extension of the shuttle program centers around a minimum requirement to recertify the vehicles in the event of additional missions \u2013 which is the second time such a reference has been made, and the second time Space Shuttle Manager John Shannon has reacting by dismissing their comments.<\/p>\n
\u201cThe ASAP Report has been released. Read it so you can be informed. This report did not mention the certification\/verification work done by the SSP since 2005,\u201d Mr Shannon noted on the latest Shuttle Standup\/Integration report \u2013 available on L2 \u2013 before citing an example of just how well the vehicles are performing.<\/p>\n
\u201cAs proof of how well the technicians are maintaining the vehicles and equipment, during the STS-129\/ULF3 mission, there were only two IFAs (In Flight Anomalies): 1) a clogged urine filter; and 2) a burned-out lightbulb. This performance indicates how well the team is doing in putting together an outstanding vehicle that performs well in flight.\u201d<\/p>\n
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![\"A2\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A215.jpg\" "\\"A2\\"")
However, with only one major effort to extend the program at the political level remaining, the possibility of extending shuttle is become less likely by the month. Mr Shannon also appeared to accept extension isn\u2019t going to happen.<\/p>\n\u201cThe State of the Union address from President Obama is January 27. The FY10 budget rollout will be February 1. There are no changes anticipated to the Shuttle plan for this year,\u201d he added on the Standup report. \u201cWe know what we have to do, and how to do it. (Mr. Shannon) expressed his pride in the SSP Team and all of the hard work it performs on a daily basis.\u201d<\/p>\n
With the three superstar vehicles now contemplating a retirement of being poked and prodded by tourists, no one will miss their house calls more than the ISS, which will have to survive on the rations of the Russian Progress, the European ATV, the Japanese HTV and the Commercial Resupply Services (CRS) partners \u2013 all of which will not come close to the upmass and downmass capability of the shuttle.<\/p>\n
Ironically, the ISS is likely to be extended to 2020, despite losing its main lifeline, along with thousands upon thousands of dedicated and world class engineers. However, there may be a silver lining in the near and distant future, as NASA is refocused away from Low Earth Orbit (LEO), with a new Heavy Lift Launcher (HLV) as its centrepiece.<\/p>\n
\u201cEmphasis is being placed on a Shuttle-derived in-line activity that is looking at a Block 1 concept that will utilize existing Shuttle assets after the end of the SSP,\u201d noted a Standup report last week. \u201cThe goal is to put some flights together and to determine a timeline and a prospective budget.\u201d<\/p>\n
As reported by NASASpaceflight.com, a \u201cspecial team\u201d was set up by NASA Administrator Charlie Bolden to evaluate all the Heavy Lifter options and alternatives to Ares V.<\/p>\n
![\"A3\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A315.jpg\" "\\"A3\\"")
Their findings have since been presented, with the Sidemount HLV losing out to the In-Line Shuttle Derived HLV, which sources claim is based on a Jupiter-241 Stretched Heavy. Members of the \u201cDirect\u201d effort met again with NASA\u2019s top management at NASA HQ just this week.<\/p>\nAs a result, the SSP has changed its main focus away from the Sidemount HLV to the In-Line concept, as noted in this week\u2019s standup report.<\/p>\n
\u201cHeavy Lift Launch Vehicle (HLV) (NASA\/JSC): The Shuttle-derived in-line activity is proceeding well. A review of how much of the MPS (Main Propulsion System) components can be utilized has been held and the results look promising.<\/p>\n
\u201cThere will be a review of how to apply Shuttle flight software to the HLV on Friday. Options for performing an early demonstration will be discussed with Mr. Shannon.\u201d<\/p>\n
While timelines and schedules for the HLV aren\u2019t likely to be known for some time, the roles this vehicle will be used for \u2013 past NASA\u2019s involvement with the ISS \u2013 remains the main question.<\/p>\n
Early indications of how NASA\u2019s forward path would be refined showed support for visiting a Near Earth Object (NEO) as a deep space mission \u2013 and as noted on NASA\u2019s internal \u201cFlexible Path\u201d evaluation presentation. This may remain the case, although very little has been heard since its section in the aforementioned presentation, bar a few documented mentions that this could be pushed back until after a Mars mission.<\/p>\n
![\"A4\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A414.jpg\" "\\"A4\\"")
What has received a large amount of political and NASA attention over recent weeks is one of the other options outlined in the presentation \u2013 for manned missions to construct a giant telescope in Geostationary orbit (GEO), and possibly as far as the region of Earth-Moon L1, before being carried to their operational location at SE L2 (Sun-Earth L2).<\/p>\nBoth the Telescopes and NEO missions would utilize Orion, a Hab\/Servicing Node, and ride with a Centaur Upper Stage.<\/p>\n
Specific mission evaluations have already started at NASA, with support at the Senate level (request was made not to name the NASA managers in this article). However, it remains uncertain if such an approach would come before, after, or even replace a mission to a NEO \u2013 although NASA\u2019s internal findings also support the priority of working towards the construction of telescopes as a priority on the roadmap.<\/p>\n
\u201cDeep-space telescope-assembly missions described in this package are \u2018even easier\u2019 and more incremental than NEO exploration, so they may provide options for a gentler and quicker start than envisioned by the Augustine Committee.\u201d<\/p>\n
Notably, all references towards the initial exploration goal of President Bush\u2019s Vision for Space Exploration (VSE) \u2013 landing on the moon and setting up a lunar base \u2013 have vanished, and threaten to disappear completely from NASA\u2019s ambitions.<\/p>\n
See also:
\nPart 1: Battle of the Heavy Lift Launchers \u2013 Monster 200mt vehicle noted
\nPart 2: Manned mission to construct huge GEO and deep space telescopes proposed
\nPart 3: NASA Flexible Path Evaluation of 2025 human mission to visit an asteriod<\/p>\nMars Orbit\/Phobos Landing:<\/p>\n
![\"A7\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A73.jpg\" "\\"A7\\"")
The big prize always has been \u2013 and continues to be \u2013 Mars. The roadmap, however, to achieve a Neil Armstrong-style footstep on the surface of the Red Planet is set to change if the Flexible Path approach is confirmed, with the preferred choice to send a human expedition into the orbit of Mars \u2013 without landing \u2013 before heading to its nearby moon of Phobos.<\/p>\n\u201cA human Mars Orbit\/Phobos Mission represents an intermediate step between human exploration missions in near-Earth space and human missions to explore the surface of Mars,\u201d opened the expansive section on the manned missions to Mars\/Phobos in the 65 page NASA internal \u201cFlexible Path\u201d presentation (available to download on L2).<\/p>\n
\u201cKey features could include demonstration of in-space hardware elements designed for Mars missions while accomplishing scientific and exploration objectives both at Mars and on Phobos.\u201d<\/p>\n
Citing an example mission, NASA managers outlined how they would approach the mission duration for the crew \u2013 which would be up to 650 days based on a short stay mission.<\/p>\n
![\"A5\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A57.jpg\" "\\"A5\\"")
\u201cThis example mission uses an \u2018short stay\u2019 trajectory (\u2018opposition class\u2019). Total mission durations for the short-stay missions range from 550-650 days, with 30 to 40 days in the vicinity of Mars. Over 95 percent of the total mission time is spent in the deep-space interplanetary environment with the balance spent in the vicinity of Mars.<\/p>\n\u201cDuration of the transit legs ranges from a minimum of 190 days and maximum in excess of 400 days. Conjunction-class missions (about 20-40 percent longer in total but with over 12x the staytime) are also feasible for a Phobos mission.\u201d<\/p>\n
As to when such a mission would be viable to launch is unknown. However, it would involve a large ramp up in the use of the HLV \u2013 with up to 15 launches of the heavy lifter to send all the elements of the Mars Transport Vehicle (MTV) into LEO for assembly.<\/p>\n
For the purpose of the presentation\u2019s example, Ares V and Ares I are illustrated \u2013 although neither are cited by name in the presentation \u2013 along with a MTV that is made up of numerous propulsive stages, a large Hab Module (CTV) and Orion.<\/p>\n
\u201cThe mission begins with the launch of the Crew Transfer Vehicle (CTV). Propulsive stages for the major in-space maneuvers are launched next. Due to the wide variability of the short stay class trajectories the number of propulsive stages varies with opportunity, as will the number of HLV launches,\u201d added the presentation.<\/p>\n
\u201cAssuming hydrogen-oxygen in-space propulsion, the number of HLV launches varies between 10 and 15. Once all of the in-space propulsive stages are assembled in LEO, the crew is launched via Orion and the crew departs for Mars.\u201d<\/p>\n
![\"A6\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A64.jpg\" "\\"A6\\"")
Incidentally, the example mission involves a fly-by of Venus on the return leg \u2013 and the closest man has ever been to the Sun \u2013 along with possible flybys of several asteroids.<\/p>\n\u201cOn arrival at Mars the crew propulsively captures into orbit and eventually maneuvers to Phobos rendezvous. After a 40 day stay in the vicinity of Mars, the crew departs for Earth return. The return leg is targeted for a Venus flyby to reduce the propulsive requirement.<\/p>\n
\u201cSince this leg likely passes inside the orbit of Venus, such a mission would include the closest approach to the Sun by a human crew. Small asteroid flyby opportunities may also exist on such trajectories. The crew can participate in science investigation of flyby objects from a unique perspective.<\/p>\n
\u201cThe Orion used to launch and board the crew is also used to return them to Earth via direct entry. The Crew Transfer Vehicle is targeted to flyby Earth and is expended in deep space.\u201d<\/p>\n
The NASA authors then focus on why they approached Mars via a \u201cPhobos-First\u201d mission, noting it was first suggested by the Augustine Committee.<\/p>\n
\u201cOur choice to include a short-stay human visit to Phobos as an example step toward humans-on-Mars is outside the framework of missions extensively analyzed by recent agency Mars mission planning, which have focused on Mars surface missions themselves.<\/p>\n
\u201cSuch a mission is suggested by the Augustine Committee as a possible element of a Flexible Path strategy, so it bears examination.<\/p>\n
\u201cAssessment of the value of such a mission compared to the risk of sending crew on a multi-year, deep-space mission is a function not only of the potential science return, inter-operation with parallel robotic Mars surface missions, and direct feed-forward to human Mars surface missions, but also of the unique technical challenges and risks it would impose, and also how \u2018fast\u2019 the program intends to get to the surface of Mars.\u201d<\/p>\n
In fact, the presentation goes on to support the idea of targeting a landing on Phobos prior to a manned mission to the surface of Mars, citing formidable challenges with the latter.<\/p>\n
![\"A9\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A91.jpg\" "\\"A9\\"")
\u201cAugustine Committee advocated a trip to orbit Mars and\/or rendezvous with its moons prior to a trip to land on Mars. Such a trip nominally lasts three years, but could be made shorter with significant delta V penalty.<\/p>\n\u201c2-yr mission (30-45 days at Mars, all-chemical propulsion) requires ~10-15 HLVs and a Venus flyby. 3-yr mission (1.5 years at Mars, all-chemical propulsion) requires ~5 HLVs. ~3 HLVs if nuclear thermal propulsion (see image left).<\/p>\n
\u201cOn the first trip to Mars, why go all that way but not land? Formidable challenges of EDL (Entry, Descent, Landing) and ISRU (in situ resource utilization), and expense of surface systems, add to an already formidable list of other challenges.<\/p>\n
\u201cHowever, landing reduces radiation and may provide gravity reconditioning. A shorter visit orbiting Mars (e.g., a 2-year Phobos mission) avoids the \u2018high bar\u2019 of a surface mission while also minimizing radiation and microgravity exposure, at the cost of more Earth launches.\u201d<\/p>\n
Interest in Phobos\/Aiding Mars Mission:<\/p>\n
Further comments are made to support a Phobos mission as a precursor to a manned mission to Mars, primarily from two standpoints; a learning curve for a future mission to Mars, and the Mars science that can be gained from Phobos.<\/p>\n
![\"A11\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A117.jpg\" "\\"A11\\"")
\u201cThe mystery of the origin of Phobos can be resolved, and its evolution since formation can be investigated by field geologists on site in contact with a larger team back on Earth. As a possible D-type (organics-rich with possible interior ice) asteroid, it offers science beyond what is readily available in the NEO population, and can shed light on the objects that delivered the initial inventory of water and organics to the surfaces of Earth and Mars,\u201d the presentation continued.<\/p>\n\u201cReturned samples would contain a record frozen very early in the formation of the solar system. The work would benefit significantly from a conjunction-class mission (540 days vs. 40 days at the target), since Phobos is a large and diverse body.<\/p>\n
\u201cPhobos has been a collector of ejected Martian surface material for billions of years. That material is a record of the history of early Mars that may not even be preserved on Mars itself due to weathering. Martian material should be readily recognizable by color for collection. These samples would be an important supplement to samples collected directly from the surface of Mars.\u201d<\/p>\n
![\"A12\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A121.jpg\" "\\"A12\\"")
Supported by robotic companions such as Rovers, the astronauts would focus on collecting science samples for return to Earth and search for water ice \u2013 all whilst in the shadow of the Red Planet.<\/p>\n\u201cOperation of Mars rovers from Earth is limited by the light time and communication opportunities to once-per-sol driving and articulation commands. From Phobos, a landing site would be visible about twice per sol for four hours each time, so on the order of four hours per sol during daylight.<\/p>\n
\u201cTwo rovers with sufficient longitudinal separation could be operated by a single astronaut during a reasonable workday. The almost zero latency would permit vastly more efficient field work and sample collection on Mars than possible if they are operated from Earth. Even joy-sticked driving would be feasible, allowing the rovers to cover much greater distances.<\/p>\n
\u201cThe ability to interact with the environment in real time would significantly improve our understanding of the geology and our ability to select samples that best reveal the physical and biological history of Mars. Samples can be launched into orbit for pickup by the crew, or for later pickup by robotic return orbiters. This work would also benefit significantly from a conjunction-class mission.<\/p>\n
\u201cThe low density of Phobos and its D-type spectrum suggests the possibility of large amounts of interior ice. Accessible ice would be a tremendous boon to later crewed Mars missions if it enables refueling in Mars orbit.\u201d<\/p>\n
![\"A14\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A141.jpg\" "\\"A14\\"")
Regardless, Phobos presents a number of Mars-like challenges to a manned mission, and certainly isn\u2019t an easy route. However, the benefit of taking on Phobos would allow NASA engineers and astronauts to learn how to approach a subsequent Mars mission by proxy.<\/p>\n\u201cOne of the significant advantages a Phobos mission would be to demonstrate many of the technical and operational approaches needed for Mars missions without yet having all the required systems, or committing the crew to a full-duration surface stay. A Phobos mission could drive and demonstrate solutions of these items.<\/p>\n
Such challenges mainly relate to the safety of the crew \u2013 which in turn would focus engineering efforts via the design of the MTV\/CTV and Orion.<\/p>\n
\u201cPassing closer than 1 AU distance to the Sun poses significant mission, vehicle design and human health issues which the mission approach must be designed for,\u201d added the presentation.<\/p>\n
\u201cRadiation Shielding: Additional shielding mass to protect from solar flares during solar maximum. Since the strength of the radiation dose is inversely proportional to\/or dose to the crew. Potential risks are higher risk of carcinogenesis, acute syndromes, CNS (central nervous system) effects and degenerative effects due to longer transits.<\/p>\n
\u201cThermal Control: Vehicle heat load increases with closer perihelion passage. Deployable sun shades are probably required for short-stay missions to shadow critical vehicle components and areas. Deployable radiators and additional active cooling loops may be required.<\/p>\n
\u201cVehicle Orientation: Due to the increased thermal and solar influence, vehicle systems including solar arrays and sunshades must be positioned relative to the sun with tighter control in order to prevent overheating.<\/p>\n
![\"A10\"](\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2010\/01\/A101.jpg\" "\\"A10\\"")
\u201cLaunch vehicle campaign: The shorter total duration of opposition-class missions comes at the expense of higher total delta V, and this varies significantly with opportunity. The net result is a need to launch more in-space propulsion elements, compared to the longer, long-stay conjunction-class missions.<\/p>\n\u201cIn addition, spending an entire Mars mission in microgravity (rather than interleaving a 500+ day stay in the 3\/8 g environment of the Mars surface) would be far outside current human micro-g experience envelope (n = 1 @14 months) no matter which trajectory option is used.<\/p>\n
\u201cMitigation might be based on a modified exercise and pharmaceutical program, or artificial-g vehicle design; both are unprecedented. Unique costs and benefits of missions similar to the example would need to be evaluated in the context of overall Flexible Path objectives.\u201d<\/p>\n
Several additional elements surrounding the technical aspect of comparing a mission to Phobos and Mars are also outlined, prior to a supportive conclusion that outlines Phobos as the best \u201clegacy\u201d for a Mars mission.<\/p>\n
\u201cA human Mars Orbit\/Phobos Mission represents an intermediate step between human exploration missions in near Earth space and human missions to explore the surface of Mars. Key features could include demonstration of inspace hardware elements designed for Mars missions while accomplishing scientific and exploration objectives both at Mars and on Phobos.<\/p>\n
\u201cAt the completion of this mission, design solutions for and demonstrations of in-space hardware elements designed for human Mars surface mission will have been accomplished, as will significant scientific and exploration objectives at Mars and Phobos. Significant such objectives include gathering and preliminary analysis of samples from both Mars and Phobos, including samples from candidate landing site for future human crews.<\/p>\n
\u201cThis mission could build on prior deep space missions by human crews in Earth-Moon space and to NEOs. It would leave a legacy of better understanding of both Mars and Phobos, along with a foundation for human missions to the surface of Mars.<\/p>\n
\u201cAchieving that legacy through such a mission would require meeting some unique challenges not needed for subsequent Mars surface missions. Key Accomplishments: Human round trip to Mars orbit. Phobos and Mars sample return for analysis in terrestrial laboratories.<\/p>\n
\u201cKey Mission Legacy: In-space portion of future Mars missions demonstrated. Ground ops and hardware processing. Deep-space crew operations. High-bandwidth communication. Planetary protection and sample analysis protocols. Some Phobos-unique challenges.\u201d<\/p>\n
A final article based on the Flexible Approach presentation will be published at the time of the first official announcement via NASA\/the President.<\/p>\n
L2 members<\/em><\/em>: Documentation \u2013 from which the above article has quoted snippets \u2013 is available in full in the related L2 sections, now over 4000 gbs in size<\/em><\/em><\/p>\n","protected":false},"excerpt":{"rendered":"
With the official opening statements on the overhaul of NASA\u2019s future expected \u201csoon\u201d, the realignment of NASA\u2019s future goals will create a Human Space Flight path that will likely stretch out for decades. The end goal remains footsteps on Mars, but the approach may involve the use of deep space and Phobos as the precursor […]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[9157,9034,367,9095,2317,8184],"class_list":["post-40886","post","type-post","status-publish","format-standard","hentry","category-news","tag-extension","tag-hlv","tag-mars","tag-mtv","tag-phobos","tag-sls-orion"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/40886"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=40886"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/40886\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=40886"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=40886"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=40886"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}