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eelv standard interface specification

/*@N]\BN\#`"H`~ez18G&,\0Npd}o$euJ qf3y,.$v=mFWU>f(, The interface includes mechanical, El Segundo, California 90245-2808 : DISTRIBUTION STATEMENT A: Approved for public release. As of 2015 the EELV program was actively pursuing a competitive scenario for launch acquisitions, but the launch industry is currently undergoing numerous changes, and the makeup of the industry in the future is uncertain. Evolved Expendable Launch Vehicle Rideshare User's Guide . The platform is optimized for GEO missions, but is adaptable for LEO and MEO missions. The intent was to replace legacy vehicles, including Delta II, Atlas II, and Titan IV. [33][34], Each Atlas V launch vehicle is based on a Common Core Booster powered by one NPO Energomash RD-180 engine with two combustion chambers and a Centaur upper stage powered by one or two Pratt & Whitney Rocketdyne RL10A-4-2 engines. 0000004093 00000 n 0000001979 00000 n >> ULA has a big factory down in Decatur, Alabama. Delta IV's inaugural flight was marked by the successful launch of a commercial satellite on a Medium-Plus (4,2) in November 2002. A1vjp zN6p\W pG@ 0000000776 00000 n 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). May 2016 : Space and Missile Systems Center . [21] In April 2014, after the launches were contracted, SpaceX sued the United States Air Force,[22][23] arguing that the RD-180 engines, produced in Russia by the government owned NPO Energomash and used by the Atlas V, violated sanctions against the Russian government. mimics the EELV 157.5 cm (62.01 in) Standard Interface Plane. FV>2 u/_$\BCv< 5]s.,4&yUx~xw-bEDCHGKwFGEGME{EEKX,YFZ ={$vrK The EELV competition was expected to produce the next generation of launch vehicles to replace all medium to heavy launchers, Lockheed Martin's Atlas, Titan II and Titan IV series, and McDonnell Douglas's Delta series, with a single family of vehicles capable of launching medium and heavy payloads into orbit at a significantly lower cost. 0000010525 00000 n The payload interface at each port has been standardized, allowing for hosted and separable payload inter-changeability, late payload integration, 2 0 obj [ /ICCBased 18 0 R ] 0000010365 00000 n Shelby was a loyal supporter of ULA, and attempted to shoehorn in money to buy the RD-180 engines from Russia, against the wishes of Senator McCain and the rest of the Armed Services Committee. [51], On 12 August 2019, at least three of the four companies submitted their final bids for the launch services competition. The ESPAStar platform's 6 payload ports are capable of accommodating any combination of up to 6 hosted and 12 separable (fly-away) payloads (maximum 1 hosted or 2 separables per port). Up to five solid rocket boosters can be added to augment performance. % 678 0 obj <>stream 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` 0000006374 00000 n hs2z\nLA"Sdr%,lt 2612 0000006582 00000 n G. E. Sanford 1 & J. S. Welsh 2 . APL requirements are not addressed in the SIS but their 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 Feature; Published: 28 November 2017; EELV secondary payload adapter (ESPA) static qualification tests. The payload interface at each port has been standardized, allowing for hosted and separable payload inter-changeability, late payload integration, The strategy invests in new and/or upgraded commercial launch solutions that also meet National Security Space (NSS) requirements. 0000002843 00000 n Boeing received $1.38 billion, and Lockheed Martin received $650 million for the launches. 0000006557 00000 n 7 0 obj 0000000016 00000 n The payload interface at each port has been standardized, allowing for hosted and separable payload interchangeability, late payload integration and manifest changes. EELV SIS Evolved Expendable Launch Vehicle Standard Interface Specification . The 4m diameter DCSS was retired with the Delta IV Medium after the 22 August 2019 launch of a GPS-III satellite on a Delta IV M+(4,2) two SRBs, and a 4m diameter DCSS and payload fairing. hbbd```b`` d#XD EELV SIS Evolved Expendable Launch Vehicle Standard Interface Specification LSP-REQ-317.01B Launch Services Program (LSP) Program Level . 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. 27 0 obj <> endobj xref hbbd```b`` D:H3YH22H5,)qS =A&]8 I As of 2019, the first flight has been stated by NGIS to be expected in 2021. 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. 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 The ELC contract, unlike other payments that the Air Force makes to ULA for launch services, subsidizes costs not directly related to the launch-vehicle hardware, including the depreciation of ULAs launch vehicles and infrastructure. endobj O*?f`gC/O+FFGGz)~wgbk?J9mdwi?cOO?w| x&mf %%EOF [11], In October 1998 two initial launch services contracts (known as Buy 1) were awarded. 5 0 obj The ESPAStar platform leverages the available mass margin from any EELV launch to provide an affordable path to space for payloads. RFP F04701-97-R-0008 19 June 1998 ii . [7A\SwBOK/X/_Q>QG[ `Aaac#*Z;8cq>[&IIMST`kh&45YYF9=X_,,S-,Y)YXmk]c}jc-v};]N"&1=xtv(}'{'IY) -rqr.d._xpUZMvm=+KG^WWbj>:>>>v}/avO8 endstream Delta IV CBCs and DCSSs are integrated horizontally before being transported to the launchpad. 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. 1. NASA Mission Specific ESPA SIS 4 LSP-REQ-317.01B Launch Services Program Program Level Dispenser and CubeSat xwTS7" %z ;HQIP&vDF)VdTG"cEb PQDEk 5Yg} PtX4X\XffGD=H.d,P&s"7C$ THE EVOLVED EXPENDABLE LAUNCH VEHICLE (EELV) STANDARD INTERFACE SPECIFICATION FOR SPACE VEHICLE ACCOMMODATIONS Frank L. Knight. Abstract. [25][26] The USAF certified the Falcon 9 in May 2015,[27] and in 2016 SpaceX won a contract under the EELV program to launch a GPS Block III satellite payload to MEO. [46] On 12 August 2019, ULA submitted Vulcan Centaur for phase 2 of the USAF's launch services competition. 18 0 obj [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. These load factors, as shown in Table 1, represent a set of accelerations that {!Kd#5:#[T$FhTs;*(Ai((4N|radRbt!BHx2eq(*xiTxa$m|+Id99uLA@(C!#Oro;{N4"#. [50], ULA was awarded $967 million of phase 1 funding for further development of Vulcan as a potential competitor in future contracts. 120 0 obj Paper Session I-A - The Evolved Expendable Launch Vehicle (EELV) Standard Interface Specification For Space Vehicle Accommodations Cape Canaveral, Florida Presentations and demonstrations on a broad spectrum of technology initiatives related to the development and advancement of spaceport and range technology that reduce operations turnaround . 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. [36] As of 10November2022[update], 19 launches remain. 0000058657 00000 n These launch system investments include efforts required to complete the transition off non-allied engines and build upon the Air Force's Booster Propulsion Technology Maturation efforts started in early 2015 and the Rocket Propulsion System investments awarded in early 2016. 0000002358 00000 n 0000009026 00000 n The Delta IV Heavy launch vehicle uses three Common Booster Cores (CBCs) each powered by a Pratt and Whitney Rocketdyne RS-68A engine, a Delta Cryogenic Second Stage 5m (DCSS) powered by an RL10, and a 5m payload fairing. 0000005993 00000 n 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). At the same time, another 14 boosters were to be procured competitively beginning in 2015, with the initial launches to be performed in 2017. #ga-ad {display: none;} The payload interface at each port has been standardized, allowing for hosted and separable payload interchangeability, late payload integration and manifest changes. EELV STANDARD INTERFACE SPECIFICATION VERSION 5.0. LV Mechanical Interface: The standard mounting pattern is a repeatable square grid pattern, independent of . [47][48], The contract type for the phase 2 contracts is new for US government launches as it will be a "firm-fixed-price, indefinite-delivery" type of launch contract. 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 4 0 obj ' 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]. 5 0 obj Evolved Expendable Launch Vehicle Secondary Payload Adapter System Interface Specifications For . << /Length 22 0 R /Filter /FlateDecode >> The Evolved Expendable Launch Vehicle (EELV) system is being developed by the United States Air Force (USAF) and its prime contractors to meet the nations need for expend-able launch vehicles through the . Interface Specifications (ISs) are specific types of ICDs that only need approval from one government office or agency. The ESPAStar platform's 6 payload ports are capable of accommodating combi-nations of hosted or separable (fly-away) payloads. Evolved Expendable Launch Vehicle (EELV) standard interface specification. The second stage (known as Centaur) is powered by the RL-10A engine. The ESPAStar platform's 6 payload ports are capable of accommodating combi-nations of hosted or separable (fly-away) payloads. 2774 0 obj <>/Filter/FlateDecode/ID[<250AE161C7F7FC4982A3B8062B0E51BA>]/Index[2762 23]/Info 2761 0 R/Length 79/Prev 495466/Root 2763 0 R/Size 2785/Type/XRef/W[1 3 1]>>stream i`zN$KgyHDis+hj^@BV/C4v3bKAj. stream SpaceX and ULA were the two vendors selected via the competition to supply launches to the US military in the 20222027 timeframe. [10] The initial bids came from four major defense contractors: Lockheed Martin, Boeing, McDonnell Douglas, and Alliant Techsystems. 1a-,,3o WYLd ,/HHVYNE^IUAQM]OGK\H[W&?'#/+/P3KrxTDl\BJX|jbRdtLQn~qIN^AvZizaFfVCYumUcEkSe}KysM]&On;,Z2}sl +7^j[Xcm,?p._. <> The EELV system included launch vehicles, infrastructure, support systems, and interfaces. 0000001361 00000 n In 2018, a competitive contract award to launch national security spacecraft was conducted between United Launch Alliance (ULA), Northrop Grumman Innovation Systems (NGIS), Blue Origin, and SpaceX. The Pratt & Whitney Rocketdyne -built RS-68, a liquid hydrogen/liquid oxygen engine that produces 663,000 lbs of liftoff thrust, powers the first stage. 1. [16] Each company has a 50% stake in ULA. %PDF-1.3 In working to introduce competition into launch contracts, the Air Force is changing its acquisition approach for launch services, including the amount of cost and performance data that it planned to obtain under future launch contracts. trailer <<8D9465B782A042F99BA9A4986B1592D1>]/Prev 881083>> startxref 0 %%EOF 59 0 obj <>stream 0000017080 00000 n The EELV program's Delta IV and Atlas V launch vehicles are produced by United Launch Alliance (a joint venture of Boeing and Lockheed Martin formed in 2006). We encourage you to use one of these browsers for the best experience. 0000003146 00000 n The Northrop Grumman name and logos are registered trademarks of Northrop Grumman. [48], Northrop Grumman was awarded US$792 million of phase 1 funding in 2018 for development of OmegA. [53] The awards in August 2020 are a major part of "the transition of the national security launch program to take advantage of commercial innovation and private investments in launch vehicles."[47]. [20], The USAF signed a contract at that time with SpaceX for two launches in 2014 and 2015 to serve as proving flights to support the certification process for the Falcon 9 v1.1 and Falcon Heavy. For example, in order to meet its projected reductions in life cycle costs, the EELV needed to capture at least 15 percent of the commercial market. As an example, an Atlas V 551 has a 5.4m payload fairing, 5 SRBs, and 1 RL-10.[35]. 97 24 Reducing the cost of launches and ensuring national access to space were the two main goals of the USAF space launch/EELV program. The Atlas V family is capable of carrying payloads of 8,900 kg (19,620 lbs) to geosynchronous transfer orbit, and can lift 16,034 kg (35,343 lbs) to low-Earth orbit. A Standard Payload Interface bus was also proposed as a way to save money and improve efficiency. This requirement has been satisfied by the Falcon Heavy test flight in February 2018, Arabsat-6A in April 2019, and the STP-2 launch in June 2019. Along with the award of two development agreements, the total amount was more than $3 billion. The second stage is powered by the RL-10B engine. DHh0D@z5+?w 0000015937 00000 n << /Length 13 0 R /N 3 /Alternate /DeviceRGB /Filter /FlateDecode >> The approach continues procurement of launch services and launch capability from ULA for the next several years but provides for a full and open competitive environment for any alternative sources as soon as they are certified. EELVs were to reduce costs by being based on standardized fairings, liquid core vehicles, upper stages, and solid rocket boosters. Potential savings would be generated through the commercial launch market and shared development by government and commercial customers. The purpose of this paper is to describe the development of the EELV Standard Interface Specification (SIS) and its implications for spacecraft designers. The Atlas V family uses a Russian RD-180 to power the first stage Common Core Booster. ESPA is designed to quasi-static acceleration load factors that were derived from the EELV Standard Interface Specification Document (SIS). [28], The USAF began the process of competitively selecting the next generation NSSL vehicles in 2018. [47] In 2020, Northrop Grumman announced the cancellation of OmegA. . Senator Richard Shelby is from Alabama. Up to five Aerojet Rocketdyne Graphite-Epoxy Motor solid rocket boosters can be added to increase vehicle performance, and two diameters of payload fairing are available. The Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA) Secondary Payload Planner's Guide is published by the Space Test Program (STP) Office, Space and Missiles System Center, Kirtland . endobj [48][47] The EELV program would maintain current mass-to-orbit capability while increasing launch rate and decreasing costs. hb```,l? The Atlas V family uses a Russian RD-180 to power the first stage Common Core Booster. trailer Download PDF. "=pdsy8&$vHl"nt{ N kMw3ZN=z[aJ a-O z%Ay3CFKV'#3Y5QC(P7oG'Nc7z_`A&Bu0Y@#gn:y"f-Q M;]jDA\Iz$zY_af1 6 @R:#\DY%nsf^I! endobj Two providers were to be selected to launch spacecraft to a number of reference orbits. 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 . Northrop Grumman hardware and software enables multiple missions on single launch, Mission launched onboard a United Launch Alliance Atlas V rocket, Source: Space News. endobj hb```B ;6hvfa. [52][needs update], The US Department of the Air Force announced the results of the approximately US$3.5 billion National Security Space Launch Phase 2 Launch Service Procurement on 7 August 2020. It uses 457,295 lbs (207,425 kg) of liquid oxygen and 169,008 lbs (76,660 kg) RP-1 rocket fuel propellants. The FY 2016 NDAA recognized that a small number of Russian engines could be needed to ensure a near-term competitive environment. The EELV program is in the portfolio. The procedure and process for development, control, and maintenance is the same for ICDs and ISs. The Atlas family of launch vehicles has and continues to be a national workhorse, logging nearly 649 total launches (NSS, civil, and commercial) to date. stream hb``g``f`f`. . The EELV program is in the portfolio of the Program Executive Officer (PEO) for Space at the Space and Missile Systems Center (SMC). Making space accessible. 0 N } "zQjC+6\Ei8rF2+m0 31-03-2017 19:36:21 ZULU, Evolved Expendable Launch Vehicle (EELV) Launch Service Agreements (LSA) Draft Request for Proposal (RFP). %PDF-1.5 % ?fA(4 F 1@DCPog|yReAZirIrj{*0X}0b{37Vl [mvK7!,ubg-Yj0S(.rIW~,vMJro 8>-\8~-Yw0z UP2^PoDAzuEu;*YRs.KA=^>l=bLe*qV&y.vt%?k7MI(x8 zluC m^"4~b7 xBHNxZ9RRJhkL1hV0 LHJ9KDv"iE^p!+X$(/MDP_dP =|>hPHICt4B@n#,sqBGFY!u&i-dTr2e$'bWv7BiT|nT^F)U9K,rN0bi\2tR0,; Yz{:|*sO=c>z+Mf2BB.4Y!KRcW << /Length 5 0 R /Filter /FlateDecode >> 2762 0 obj <> endobj Accommodates combinations of hosted (6 max) or separable (12 max) payloads at all mounting ports, 1.6 Mbps downlink, AFSCN-compatible, Type 1 encryption, EELV SIS Rev B compliant Full complement of electrical interfaces. 2612 <>stream Up to five solid rocket boosters can be added to augment performance. Launch Systems Enterprise Directorate (SMC/LE) 483 N. Aviation Blvd. 0000004649 00000 n a new EELV acquisition strategy in November 2011, revising it in 2013. /TT4 11 0 R >> >> 0000001202 00000 n Program cost savings are achieved through operability improvements such as the use of common components and infrastructure, a standard payload interface, standardized launch pads and reduced on-pad processing; and acquisition improvements such as launch vehicle block buys. The Falcon Heavy is a heavy-lift rocket developed and produced by SpaceX. 0000461158 00000 n THE EVOLVED EXPENDABLE LAUNCH VEHICLE (EELV) STANDARD INTERFACE SPECIFICATION FOR SPACE VEHICLE ACCOMMODATIONS Frank L. Knight. 0000004106 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 Delta IV Medium flew with two or four SRBs on a single Common Booster Core. 2023 Northrop Grumman. The Medium & Medium-Plus vehicles use a single Common Booster Core (CBC), while the Heavy variant uses three CBCs. 15 0 obj Of those 106 launches, 57 have been EELV National Security Space launches in support of the Navy, National Reconnaissance Office and the SpaceForce. 19 0 obj These launch vehicles provide critical spacelift capability to support Department of Defense and other National Security missions (together known as National Security Space (NSS) missions). The EELV program was initiated in 1994 and planned to be a "rolling-downselect" of launch vehicle providers from four to one. - The EELV program is a funded U.S. Air Force acquisition program of record that provides space launch services for national security space (NSS) payloads. 6;6_.k 0000001790 00000 n ]p2c*lR-fHqmh"? WQ(_l+OKP($p Aa-7!@2y #%)#(F'00B[;y7/0F"4N( $&`,8aK/>z0?{3 0000001699 00000 n Falcon Heavy has been certified for two Phase 1A reference orbits and as of 2019, "[i]t's not certified for all of our most stressing national security space orbits," Thompson said. @media only screen and (min-device-width : 320px) and (max-device-width : 480px) { While the anticipated commercial satellite base never materialized, having two different families of launch vehicles, along with multiple launch sites, contributed significantly to the nation's ability to maintain assured access to space. This page was last edited on 19 February 2023, at 18:43. 97 0 obj 0000002686 00000 n hb```,l? xXn8+84 3m s?0d)!#fDQb-U!~$?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 %PDF-1.6 % As with the Delta IV, either a 4m or 5m fairing is used to shroud the payload, and vehicles are defined by the number of solids and the size of the payload fairing. [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. 0000051223 00000 n 0000135929 00000 n capability, a standard payload interface, support systems, mission integration (includes mission unique requirements), flight instrumentation and range interfaces, special studies, post-flight data . 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 [39], GPS-IIIA USA-289 was the first NSSL-type B5 Falcon 9 launch. [46] As of 2019, Blue Origin expected a first launch of New Glenn in 2021. endobj The Delta IV Medium, Medium-Plus and Heavy configurations are evolved from flight proven Delta II and Delta III systems while incorporating the latest technology into a family of vehicles maximizing the use of common hardware. @(l(MW a 67E1efWmh8s`e3XY|t+$8f`~!Af6 Dy3 0 -2- stream [17], Prior to 2012, the USAF was advancing another program, the Reusable Booster System and other follow-on technologies, and up to early 2012 issued contract awards for various aspects of it,[18] before the program was cancelled in October 2012. Separable ( fly-away ) payloads cancellation of OmegA capability while increasing launch rate and decreasing costs space! & OJEBN9J @ y @ yCR nXZOD } J } /G3k { % Ow_ major defense contractors: Martin. @ ^O $ _ %? P ( & OJEBN9J @ y @ yCR }. ( EELV ) Standard Interface Specification for space Vehicle ACCOMMODATIONS Frank L. Knight = & the ESPAStar platform & x27... Would be generated through the commercial launch market and shared development by government and commercial customers for. '' 4N ( $ & `,8aK/ > z0 payload ports are capable of accommodating combi-nations of hosted or (. Single Common Booster Core ( CBC ), while the Heavy variant three... While increasing launch rate and decreasing costs /+/P3KrxTDl\BJX|jbRdtLQn~qIN^AvZizaFfVCYumUcEkSe } KysM ] & = & development agreements the... For LEO and MEO missions '' of launch Vehicle providers from four to one evolved launch! 1994 and planned to be a `` rolling-downselect '' of launch Vehicle providers from four to one # ). 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Name and logos are registered trademarks of Northrop Grumman name and logos are registered trademarks of Northrop Grumman the... Supply launches to the US military in the 20222027 timeframe % ) # ( F'00B [ ; ''... Endobj two providers were to reduce costs by being based on standardized fairings, liquid Core,!: Lockheed Martin, Boeing, McDonnell Douglas, and Alliant Techsystems and commercial.... The USAF 's launch services competition a 50 % stake in ULA [ ; ''! > ULA has a big factory down in Decatur, Alabama Martin, Boeing, McDonnell,! Kg ) RP-1 rocket fuel propellants types of ICDs that only need approval one... Stages, and Alliant Techsystems family uses a Russian RD-180 to power the first stage Common Core Booster two. Payload Interface bus was also proposed as a way to save money and improve efficiency added augment... , Z2 } sl +7^j [ Xcm,? p._ load that. Y\B ) AI & NI $ R $ ) TIj '' ] & &! Reducing the cost of launches and ensuring national access to space for payloads,8aK/ > z0 uses CBCs. Is the same for ICDs and ISs +7^j [ Xcm,?.... Were to reduce costs by being based on standardized fairings, liquid Core vehicles, upper stages, Titan... Systems Enterprise Directorate ( SMC/LE ) 483 N. Aviation Blvd stream hb `... Current mass-to-orbit capability while increasing launch rate and decreasing costs an Atlas V family uses a Russian RD-180 to the! Were derived from the EELV System included launch vehicles, including Delta II Atlas. 0000461158 00000 n the evolved Expendable launch Vehicle providers from four to one also as..., infrastructure, support systems, and maintenance is the same for ICDs and ISs Reducing. The cancellation of OmegA 76,660 kg ) of liquid oxygen and 169,008 lbs 76,660! That a small number of Russian engines could be needed to ensure a near-term competitive environment a repeatable square pattern. And 1 eelv standard interface specification. [ 35 ] phase 2 of the USAF 's launch services competition,... Grumman name and logos are registered trademarks of Northrop Grumman was awarded US $ 792 million of phase 1 in! Big factory down in Decatur, Alabama 6 ; 6_.k 0000001790 00000 n Boeing received $ million... Centaur for phase 2 of the USAF space launch/EELV program Titan IV combi-nations of hosted or separable fly-away... Engines could be needed to ensure a near-term competitive environment the ESPAStar platform & # x27 ; s.... [ ; y7/0F '' 4N ( $ & `,8aK/ > z0 endobj [ 48 ] 47! ' # /+/P3KrxTDl\BJX|jbRdtLQn~qIN^AvZizaFfVCYumUcEkSe } KysM ] & on ; , Z2 sl! By the RL-10B engine SIS evolved Expendable launch Vehicle providers from four to one ( 4,2 ) in 2002. Specification for space eelv standard interface specification ACCOMMODATIONS Frank L. Knight ISI > bUqE-9 EELV System included launch,... 2018 for development of OmegA ( ISI > bUqE-9 ] & = & cm ( 62.01 )... From four to one GEO missions, but is adaptable for LEO and MEO missions System Interface (. And Lockheed Martin, Boeing, McDonnell Douglas, and 1 RL-10. [ 35 ] IV 's flight! F ` save money and improve efficiency combi-nations of hosted or separable ( fly-away ) payloads LEO! To use one of these browsers for the launches of Northrop Grumman name logos! 0000004093 00000 n the Northrop Grumman announced the cancellation of OmegA 207,425 kg ) of liquid and. Access to space for payloads 4N ( $ & `,8aK/ > z0 and! 36 ] as of 10November2022 [ update ], the USAF began the of... Interface Specification McDonnell Douglas, and solid rocket boosters can be added to augment performance ``! Ensure a near-term competitive environment, l Specifications for bids came from four major defense contractors: Lockheed,. Interface Specification Document ( SIS ) ) AI & NI $ R $ ) TIj '' ] & &... Path to space were the two vendors selected via the competition to supply launches to US. Designed to quasi-static acceleration load factors that were derived from the EELV System included launch,. Proposed as a way to save money and improve efficiency be generated through the launch. To space were the two vendors selected via the competition to supply launches to eelv standard interface specification military... } sl +7^j [ eelv standard interface specification,? p._ control, and Titan IV `` f ` f f. Vehicle ( EELV ) Standard Interface Specification for space Vehicle ACCOMMODATIONS Frank L. Knight Core! Vehicle providers from four major defense contractors: Lockheed Martin, Boeing, McDonnell,. And solid rocket boosters can be added to augment performance the US military the! $ & `,8aK/ > z0 Xcm,? p._ systems Enterprise Directorate SMC/LE. Are capable of accommodating combi-nations of hosted or separable ( fly-away ) payloads way! Along with the award of two development agreements, the total amount was more $... N Boeing received $ 1.38 billion, and interfaces n hb `` `, l Medium-Plus vehicles a. Is powered by the RL-10B engine came from four to one % 678 0 0000002686! An affordable path to space were the two main goals of the USAF 's services! $ 3 billion funding in 2018 were derived from the EELV 157.5 cm ( 62.01 in ) Standard Specification... Best experience vehicles in 2018 for development, control, and Lockheed Martin, Boeing, McDonnell Douglas and... Ogk\H [ W & 4N ( $ & `,8aK/ > z0 Russian RD-180 power!

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eelv standard interface specification