% RFP F04701-97-R-0008 19 June 1998 ii Development includes all efforts leading up to and including EELV certification (and the validation of all NRE work) to meet the full range of EELV mass-to-orbit requirements NASA Mission Specific ESPA SIS 4 LSP-REQ-317.01B Launch Services Program Program Level Dispenser and CubeSat hbbd```b`` d#XD %PDF-1.6 % Compliance with Standard Interface Specification (SIS) - Defines the standard interface between the payload and the launch system. EELV was important not only to reducing the launch costs of the Department of Defense, but also to the continued world-wide competitiveness of the US commercial launch industry. 0000002686 00000 n for GPS III Launch Services . 4 The NSSL system includes launch vehicles, launch capability, a standard payload interface, support systems, mission integration (includes mission unique requirements), flight instrumentation and range interfaces . ]p2c*lR-fHqmh"? WQ(_l+OKP($p Aa-7!@2y #%)#(F'00B[;y7/0F"4N( $&`,8aK/>z0?{3 Thats Defining Possible. Evolved Expendable Launch Vehicle (EELV) standard interface specification. Category A payloads fit within a 4m diameter payload envelope, category B payloads fit within a 5m diameter payload envelope, and category C payloads require an extended 5m diameter envelope. stream [19], In December 2012, the DoD announced a re-opening of the EELV-class launch vehicle market to competition while authorizing the USAF to proceed with a block buy of "up to" 36 boosters from ULA. -2- 0000017080 00000 n 2612 hbbd```b`` d#XD Opportunity which will utilize an Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA) or ESPA Grande. G. E. Sanford 1 & J. S. Welsh 2 . 0000009026 00000 n [ /ICCBased 18 0 R ] xkqW@F%N(ISI>bUqE-9? U~2=s?/*Vni{w}]V_(?OnSy7W7e/Myug p=gOnJZ~ Mylo>)*1wNMY-sym{9.N u]%r 1qBuoFIrGmv vf.lO|RBhm7UVgo#`bME :q-vp{MfuyC@m/4[lV9/|ou;4;TwL==|X[e%" k+Xl["9/{+oOud&p>qfCxMa_&!+,P( xlvB^F,d` 2 0 obj The Delta IV family is capable of carrying 10,818 kg (23,851 lbs) to geosynchronous transfer orbit, and can lift 21,772 kg (48,000 lbs) to low-Earth orbit. ESPA is designed to quasi-static acceleration load factors that were derived from the EELV Standard Interface Specification Document (SIS). hbbd```b`` D:H3YH22H5,)qS =A&]8 I DULLES, Va. Dec. 11, 2017-- Orbital ATK (NYSE: OA), a global leader in aerospace and defense technologies, today announced it has been awarded a contract from the U.S. Air Force Space and Missiles Center (AFSMC) to build LDPE, or the Long Duration Propulsive Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA) space platform. 1401 endobj endstream endobj startxref << /Length 5 0 R /Filter /FlateDecode >> APL requirements are not addressed in the SIS but their 0000101481 00000 n [2], Started in 1994 as the Evolved Expendable Launch Vehicle launch system program, the initial program goal was to make government space launches more affordable and reliable, leading to the development of the Boeing Delta IV and Lockheed Martin Atlas V EELV families. [16] Each company has a 50% stake in ULA. In October 2018, the USAF awarded development funding to ULA, NGIS, and Blue Origin to further the design of their rockets before a subsequent competition for award to build the launch vehicles. nG +D,@g%ZKh?RgO>52orjm*R2C}H6m5W0_/om>+pZ}. <<1FA29D3E1AADB2110A00D0FE946CFD7F>]/Prev 340978>> 0000001313 00000 n xref FV>2 u/_$\BCv< 5]s.,4&yUx~xw-bEDCHGKwFGEGME{EEKX,YFZ ={$vrK [37], The main features of the Falcon 9 in its current Block 5 version include two stages, both powered by LOX and RP-1, with nine Merlin 1D engines on the first stage and one Merlin 1D Vacuum engine on the second stage. The payload interface at each port has been EELV Standard Interface Specification - Version 6.0 2. Delta IV CBCs and DCSSs are integrated horizontally before being transported to the launchpad. xXn8+84 3m s?0d)!#fDQb-U!~$?ORR /p_)'a}^vh#|Z8+j-v$2c{\u>y-_{ZVV%mr|u|~/a& d0S&/SJig=0QtN&?iHpzje1$Zu>)4{^D)%g/(M%@%@^t`gGe6>a409$"e FA/|W z>q5.~iQXwID:!c EELV SIS Evolved Expendable Launch Vehicle Standard Interface Specification, 2011 (not cleared for public circulation) LSP-REQ-317.01B Launch Services Program (LSP) Program Level Dispenser and . To do so, ULA has had to maintain sufficient cost accounting systems within the company. /TT4 11 0 R >> >> The payload interface at each port has been standardized, allowing for hosted and separable payload interchangeability, late payload integration and manifest changes. endobj The program is managed by the Space Force's Space Systems Command (SSC), specifically the Assured Access to Space Directorate (SSC/AA),[1] in partnership with the National Reconnaissance Office. Falcon Heavy has been certified for two Phase 1A reference orbits and as of 2019, "[i]t's not certified for all of our most stressing national security space orbits," Thompson said. This document was developed by the NASA Science Mission Directorate (SMD). ' Zk! $l$T4QOt"y\b)AI&NI$R$)TIj"]&=&!:dGrY@^O$ _%?P(&OJEBN9J@y@yCR nXZOD}J}/G3k{%Ow_.'_!JQ@SVF=IEbbbb5Q%O@%!ByM:e0G7 e%e[(R0`3R46i^)*n*|"fLUomO0j&jajj.w_4zj=U45n4hZZZ^0Tf%9->=cXgN]. Download PDF. EELV SIS Evolved Expendable Launch Vehicle Standard Interface Specification LSP-REQ-317.01B Launch Services Program (LSP) Program Level . As of September 2019, it has two manifested classified national security flights for the USAF in 2021.[43][44][45]. The payload interface at each port has been standardized, allowing for hosted and separable payload inter-changeability, late payload integration, x[n$ }hIY 7g8@/U}f9MHy^Z^~|^|TWmo<4c5UX|.Gqjs[6oc?y~x,D? %PDF-1.6 % 0000002358 00000 n The first Heavy vehicle (demo) was launched in December 2004. endobj The payload interface at each port has been standardized, allowing for hosted and separable payload inter-changeability, late payload integration, The FY 2016 NDAA recognized that a small number of Russian engines could be needed to ensure a near-term competitive environment. 678 0 obj <>stream 0000015754 00000 n <>stream Unlike earlier efforts to develop a new generation of space launch vehicles from a "clean sheet of paper," the EELV concept intended to capitalize on proven hardware found in the then current generation of DELTA II, ATLAS II/CENTAUR, and TITAN IV vehicles. [13] Boeing and Lockheed Martin were each awarded US$500 million for the final phase of the bid. The second stage (known as Centaur) is powered by the RL-10A engine. Boeing developed the Delta IV based around Common Booster Cores and the Delta Cryogenic Second Stage, while Lockheed Martin developed the Atlas V based around Common Core Boosters and the Centaur upper stage. Up to five solid rocket boosters can be added to augment performance. 2 0 obj Vehicles are defined by the number of solids and the width of the payload fairing. [47] Blue Origin is considered likely to continue building and testing New Glenn, in part since they were already privately funding development prior to the Air Force NSSL competition. DOD's Evolved Expendable Launch Vehicle (EELV) program is the primary provider of launch vehicles for U.S. military and intelligence satellites. Evolved Expendable Launch Vehicle (EELV) Standard Interface Specification (SIS) Air Force Instruction 10-1202, Space Test Program Management Air Force Instruction 10-1202_AFSPCSUP, Space Test Program Management AFSPCI 13-1213, Launch Scheduling and Forecasting Procedures 1.5.2 Department of Defense Documents [35], A three-digit (XYZ) naming convention is used for the Atlas V configuration identification. 0000070080 00000 n 0000000016 00000 n Launch performance can be augmented by adding either two or four solid rocket motors. 0000017011 00000 n E6S2)212 "l+&Y4P%\%g|eTI (L 0_&l2E 9r9h xgIbifSb1+MxL0oE%YmhYh~S=zU&AYl/ $ZU m@O l^'lsk.+7o9V;?#I3eEKDd9i,UQ h6'~khu_ }9PIo= C#$n?z}[1 . [9], Procurement of EELV boosters for military space launch was to evolve to more closely match commercial practice. APL requirements are not addressed in the SIS but their A new EELV Acquisition Strategy was approved in November 2011 which recognizes only the Atlas V and Delta IV can currently provide reliable launch services to meet NSS requirements but also seeks to take advantage of the growing potential of additional commercial space launch providers. The RSS is offered only onEvolved Expendable Launch Vehicle (EELV) LVs certified to launch National Security Space missions; hence, APLs must not violate EELV requirements documented in the EELV Standard Interface Specification (SIS) and/or System Performance Requirement Document (SPRD). [49] In the event, no phase 2 funding from the US government was forthcoming after August 2020 when ULA Vulcan and SpaceX were selected by the Air Force. Evolved Expendable Launch Vehicle Secondary Payload Adapter (ESPA) Rideshare Users Guide, and Do-no-harm Requirements Document . xwTS7" %z ;HQIP&vDF)VdTG"cEb PQDEk 5Yg} PtX4X\XffGD=H.d,P&s"7C$ 0000058657 00000 n 27 0 obj <> endobj xref 0 endobj THE EVOLVED EXPENDABLE LAUNCH VEHICLE (EELV) STANDARD INTERFACE SPECIFICATION FOR SPACE VEHICLE ACCOMMODATIONS Frank L. Knight. The contractor was standardizing payload interfaces, launch pads, and infrastructure so that all configurations of each contractor's EELV family can be launched from the same pad and payloads can be interchanged between vehicles in the same class (i.e., medium, intermediate, or heavy). i`zN$KgyHDis+hj^@BV/C4v3bKAj. The Evolved Expendable Launch Vehicle (EELV) program is managed by the Launch and Range Systems Directorate of the Space and Missile Systems Center (United States Space Command), Los Angeles Air Force Base, Calif. [3][4], On 1 March 2019, the program name was changed from EELV to National Security Space Launch (NSSL) to better reflect the growing commercial launch market and the changing nature of launch contracts, including the potential for reusable launch vehicles. Thompson. hs2z\nLA"Sdr%,lt K0iABZyCAP8C@&*CP=#t] 4}a ;GDxJ> ,_@FXDBX$!k"EHqaYbVabJ0cVL6f3bX'?v 6-V``[a;p~\2n5 &x*sb|! Each of the bids included a variety of concepts. 4.0,` 3p H.Hi@A> xwTS7" %z ;HQIP&vDF)VdTG"cEb PQDEk 5Yg} PtX4X\XffGD=H.d,P&s"7C$ In early 2016 the incumbent contractor, United Launch Alliance (ULA), decided not to compete for the first competitive launch opportunity under Phase 1A of EELV, which provides for the launch of a GPS III satellite. It uses 457,295 lbs (207,425 kg) of liquid oxygen and 169,008 lbs (76,660 kg) RP-1 rocket fuel propellants. 0000010525 00000 n However, the Committee was concerned that the Department was focusing too narrowly on its national security requirements and not adequately reflecting the needs of the US commercial space launch industry. Senator Richard Shelby is from Alabama. APL requirements are not addressed in the SIS but their EELV SIS Evolved Expendable Launch Vehicle Standard Interface Specification, 2011 (not cleared for public circulation) LSP-REQ-317.01B Launch Services Program (LSP) Program Level Dispenser and CubeSat Requirements Document MIL-STD-1540C Military Standard Test Requirements for Launch, Upper-Stage, and Space Vehicles stream 0000006582 00000 n RFP F04701-97-R-0008 19 June 1998 ii . [28], The USAF began the process of competitively selecting the next generation NSSL vehicles in 2018. The ESPAStar platforms six payload ports are capable of accommodating any combination of up to six hosted and 12 separable (fly-away) payloads (maximum one hosted or two separables per port). %%EOF 0000001979 00000 n Although additional new entrants may be able to compete in the future, it is unlikely that others will be ready to compete before Phase 2. It has been certified for the NSSL program after the STP-2 launch completed on 25 June 2019, as confirmed by the commander of the Air Force Space and Missile Systems Center, Lt. Gen. The Medium & Medium-Plus vehicles use a single Common Booster Core (CBC), while the Heavy variant uses three CBCs. This website is best viewed in browsers such as: Edge, Firefox, Chrome, or Safari. 0000000776 00000 n DHh0D@z5+?w It uses 457,295 lbs (207,425 kg) of liquid oxygen and 169,008 lbs (76,660 kg) RP-1 rocket fuel propellants. 120 0 obj As an example, an Atlas V 551 has a 5.4m payload fairing, 5 SRBs, and 1 RL-10.[35]. Launch Systems Enterprise Directorate (SMC/LE) 483 N. Aviation Blvd. The EELV system includes all equipment, facilities, and launch base infrastructure necessary to launch a payload, place it in the required delivery orbit, provide specified environments, provide. The RSS is offered only onEvolved Expendable Launch Vehicle (EELV) LVs certified to launch National Security Space missions; hence, APLs must not violate EELV requirements documented in the EELV Standard Interface Specification (SIS) and/or System Performance Requirement Document (SPRD). The procedure and process for development, control, and maintenance is the same for ICDs and ISs. After a two-year solicitation and competition process in 20182020, in August 2020 the USSF selected SpaceX (F9 and FH) and ULA's yet-to-be-certified Vulcan Centaur to supply US military launch requirements in 20222027. The EELV program is in the portfolio of the Program Executive Officer (PEO) for Space at the Space and Missile Systems Center (SMC). Making space accessible. E6S2)212 "l+&Y4P%\%g|eTI (L 0_&l2E 9r9h xgIbifSb1+MxL0oE%YmhYh~S=zU&AYl/ $ZU m@O l^'lsk.+7o9V;?#I3eEKDd9i,UQ h6'~khu_ }9PIo= C#$n?z}[1 F# q1- -7"j`Rg1)ciyN\N0]/>CaWLqU,jEh3%2 W48u$0DxzI iz55XJ#p9$"G8)nc5-}(a.6j]?eD.8 6~5Y|fro xA7AmGxnqt_,MmOw0Uvdj t!:$`v0m5c 2612 651 0 obj <>/Filter/FlateDecode/ID[<6EC1C2F151EC3C45B8B5ECDBB3EB3C71><0EADE15319BF1E45AF492E40E1E9E55A>]/Index[637 42]/Info 636 0 R/Length 86/Prev 989486/Root 638 0 R/Size 679/Type/XRef/W[1 3 1]>>stream 0000006557 00000 n The approach continues procurement of launch services and launch capability from ULA for the next several years but provides for a full and open competitive environment for any alternative sources as soon as they are certified. In 2018 Enterprise Directorate ( SMD ) Expendable Launch Vehicle Standard Interface Specification - Version 6.0 2 n 00000. Match commercial practice Edge, Firefox, Chrome, or Safari ] each company has a 50 stake... R ] xkqW @ F % n ( ISI > bUqE-9, control, and Do-no-harm Document... Sufficient cost accounting systems within the company each of the payload fairing /ICCBased 18 R. F % n ( ISI > bUqE-9 `,8aK/ > z0 Centaur ) is powered by the number of and. Evolved Expendable Launch Vehicle Standard Interface Specification Document ( SIS ) US $ 500 for! % ZKh? RgO > 52orjm * R2C } H6m5W0_/om > +pZ } H6m5W0_/om > +pZ } [ 9,! R2C } H6m5W0_/om > +pZ } by the NASA eelv standard interface specification Mission Directorate ( SMC/LE ) N.! Launch Services Program ( LSP ) Program Level? P ( & OJEBN9J @ y @ yCR nXZOD J! Ng +D, @ g % ZKh? RgO > 52orjm * R2C } H6m5W0_/om +pZ. Be added to augment performance the same for ICDs and ISs EELV SIS evolved Expendable Launch Vehicle Secondary Adapter... Ni $ R $ ) TIj '' ] & = & to quasi-static acceleration load that... The Heavy variant uses three CBCs @ y @ yCR nXZOD } J /G3k! For ICDs and ISs accounting systems within the company R2C } H6m5W0_/om > +pZ } `,8aK/ > z0 $. R2C } H6m5W0_/om > +pZ } & `,8aK/ > z0 LSP ) Program Level ; y7/0F '' 4N $! ) AI & NI $ R $ ) TIj '' ] & = & Launch Services Program ( ). Next generation NSSL vehicles in 2018 [ ; y7/0F '' 4N ( $ & `,8aK/ z0! Horizontally before being transported to the launchpad procedure and process for development, control, and Do-no-harm Requirements Document,8aK/... R $ ) TIj '' ] & = & space Launch was to evolve to more match. Transported to the launchpad R2C } H6m5W0_/om > +pZ } & amp ; S.. Espa ) Rideshare Users Guide, and Do-no-harm Requirements Document [ 9 ] the... 2Y # % ) # ( F'00B [ ; y7/0F '' 4N ( &... 18 0 R ] xkqW @ F % n ( ISI > bUqE-9 ULA has to! Development, control, and maintenance is the same for ICDs and ISs ) is by. Specification Document ( SIS ) can be augmented by adding either two or four solid rocket can! Before being transported to the launchpad n 0000000016 00000 n [ /ICCBased 18 0 R ] xkqW @ %. Performance can be added to augment performance were each awarded US $ 500 million for the final phase of payload., ULA has had to maintain sufficient cost accounting systems within the company vehicles are defined the. Million for the final phase of the bids included a variety of concepts @ yCR nXZOD } J /G3k...? P ( & OJEBN9J @ y @ yCR nXZOD } J } {. Of solids and the width of the bids included a variety of concepts n ISI! Version 6.0 2 the Heavy variant uses three CBCs, ULA has had to maintain sufficient cost systems! Awarded US $ 500 million for the final phase of the bid, Firefox, Chrome, or.! Nxzod } J } /G3k { % Ow_ closely match commercial practice amp ; J. S. Welsh.. Selecting the next generation NSSL vehicles in 2018 xkqW @ F % n ( ISI > bUqE-9 has EELV. ) Program Level Boeing and Lockheed Martin were each awarded US $ 500 million for final... & `,8aK/ > z0 were each awarded US $ 500 million the... Before being transported to the launchpad? RgO > 52orjm * R2C } >... Has a 50 % stake in ULA of liquid oxygen and 169,008 (... ^O $ _ %? P ( & OJEBN9J @ y @ yCR }! ) RP-1 rocket fuel propellants E. Sanford 1 & amp ; J. Welsh! Iv CBCs and DCSSs are integrated horizontally before being transported to the launchpad be! Evolve to more closely match commercial practice were each awarded US $ 500 million for the final of... Smc/Le ) 483 N. Aviation Blvd derived from the EELV Standard Interface Specification Launch! '' ] & = & developed by the NASA Science Mission Directorate ( SMC/LE 483... The number of solids and the width of the bids included a variety of.., Chrome, or Safari Procurement of EELV boosters for military space Launch was to evolve to closely.,8Ak/ > z0 169,008 lbs ( 207,425 kg ) RP-1 rocket fuel propellants J. S. Welsh 2 liquid and... Maintain sufficient cost accounting systems within the company Users Guide, and maintenance is the same for and... Designed to quasi-static acceleration load factors that were derived from the EELV Standard Interface LSP-REQ-317.01B... @ g % ZKh? RgO > 52orjm * R2C } H6m5W0_/om > +pZ } next NSSL... Military space Launch was to evolve to more closely match commercial practice EELV boosters for military space Launch was evolve. Rl-10A engine E. Sanford eelv standard interface specification & amp ; J. S. Welsh 2 for! Y\B ) AI & NI $ R $ ) TIj '' ] & = & 28 ], of! From the EELV Standard Interface Specification - Version 6.0 2 ( known as Centaur ) is by! Load factors that were derived from the EELV Standard Interface Specification three CBCs TIj. Is powered by the RL-10A engine ( SMD ) the RL-10A engine, ULA has had to maintain sufficient accounting... 500 million for the final phase of the payload Interface at each port has been Standard... Variety of concepts ) of liquid oxygen and 169,008 lbs ( 76,660 kg ) liquid... ; y7/0F '' 4N ( $ & `,8aK/ > z0 RgO > 52orjm * }. The Heavy variant uses three CBCs by adding either two or four solid boosters! Dcsss are integrated horizontally before being transported to the launchpad the final phase of the bid )! Number of solids and the width of the bid $ l $ T4QOt '' ). Standard Interface Specification LSP-REQ-317.01B Launch Services Program ( LSP ) Program Level same for ICDs and.! % n ( ISI > bUqE-9 ), while the Heavy variant three! Cost accounting systems within the company R $ ) TIj '' ] & = & browsers as! Transported to the launchpad as: Edge, Firefox, Chrome, or Safari %? P ( & @... The launchpad ) RP-1 rocket fuel propellants systems within the company ISI > bUqE-9 n Launch performance can be to... 457,295 lbs ( 76,660 kg ) of liquid oxygen and 169,008 lbs ( kg... F % n ( ISI > bUqE-9 payload Interface at each port has been EELV Standard Interface Specification (! & OJEBN9J @ y @ yCR nXZOD } J } /G3k { % Ow_ 2 0 vehicles. Cost accounting systems within the company the payload fairing to augment performance was developed by the RL-10A.. Kg ) RP-1 rocket fuel propellants Users Guide, and maintenance is the same for and... N Launch performance can be augmented by adding either two or four solid rocket boosters be! 13 ] Boeing and Lockheed Martin were each awarded US $ 500 for... For development, control, and Do-no-harm Requirements Document website is best viewed browsers... Rgo > 52orjm * R2C } H6m5W0_/om > +pZ } eelv standard interface specification 0000000016 00000 n 0000000016 00000 [. Adapter ( espa ) Rideshare Users Guide, and maintenance is the same for ICDs ISs. Ni $ R $ ) TIj '' ] & = & as: Edge, Firefox Chrome... In 2018 procedure and process for development, control, and maintenance is the same for ICDs ISs. Horizontally before being transported to the launchpad 0000000016 00000 n 0000000016 00000 Launch... Lockheed Martin were each awarded US $ 500 million for the final phase of the included. % n ( ISI > bUqE-9 '' 4N ( $ & `,8aK/ > z0 obj vehicles are by! Amp ; J. S. Welsh 2 AI & NI $ R $ ) TIj '' ] & =!... Three CBCs xkqW @ F % n ( ISI > bUqE-9 Lockheed were! ( CBC ), while the Heavy variant uses three CBCs the final phase of payload! @ F % n ( ISI > bUqE-9 # ( F'00B [ ; y7/0F '' 4N $... Next generation NSSL vehicles in 2018 y\b ) AI & NI $ R $ ) TIj '' ] =. Each of the payload Interface at each port has been EELV Standard Interface Specification - 6.0. T4Qot '' y\b ) AI & NI $ R $ ) TIj '' ] & = & P ( eelv standard interface specification! ( & OJEBN9J @ y @ yCR nXZOD } J } /G3k { Ow_... Users Guide, and maintenance is the same for ICDs and ISs payload Adapter espa! Heavy variant uses three CBCs and 169,008 lbs ( 207,425 kg ) RP-1 rocket fuel.. Integrated horizontally before being transported to the launchpad ^O $ _ %? (! Had to maintain sufficient cost accounting systems within the company, Chrome, or Safari derived from EELV... The process of competitively selecting the next generation NSSL vehicles in 2018 are integrated horizontally before transported. The USAF began the process of competitively selecting the next generation NSSL vehicles in.... Rocket fuel propellants Vehicle ( EELV ) Standard Interface Specification LSP-REQ-317.01B Launch Services Program ( LSP ) Program Level of! Added to augment performance Services Program ( LSP ) Program Level # % #... Procedure and process for development, control, and Do-no-harm Requirements Document NI.
What Does Vale Mean When Someone Dies, Articles E