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3p H.Hi@A> Abstract. 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. Feature; Published: 28 November 2017; EELV secondary payload adapter (ESPA) static qualification tests. endobj As of 2019, the first flight has been stated by NGIS to be expected in 2021. 0000006374 00000 n
Steady production rates, long-term commitments and opportunities for competition are among the means to achieve this goal. The payload interface at each port has been standardized, allowing for hosted and separable payload interchangeability, late payload integration and manifest changes. /TT2 9 0 R /TT6 13 0 R /TT10 17 0 R /TT4 11 0 R >> >> Development is defined as all activities from initial concept up to, but not including, production. 0000003910 00000 n
QUk{vv7m-C4W>!z~>X#Nz---1GjN. Up to five solid rocket boosters can be added to augment performance. The USAF began the EELV program in 1994, following many years of government-funded studies into improved systems and architecture. /*@N]\BN\#`"H`~ez18G&,\0Npd}o$euJ qf3y,.$v=mFWU>f(, trailer 2762 0 obj
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Launch performance can be augmented by adding either two or four solid rocket motors. 0000015937 00000 n
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). Senator Richard Shelby is from Alabama. 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. 637 0 obj
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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. %PDF-1.4
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[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. Along with the award of two development agreements, the total amount was more than $3 billion. 12 0 obj 0000003146 00000 n
15 0 obj Abstract. APL requirements are not addressed in the SIS but their hb```,l? Compliance with Standard Interface Specification (SIS) - Defines the standard interface between the payload and the launch system. May 2016 : Space and Missile Systems Center . On this Wikipedia the language links are at the top of the page across from the article title. The platform is optimized for GEO missions, but is adaptable for LEO and MEO missions. El Segundo, California 90245-2808 : DISTRIBUTION STATEMENT A: Approved for public release. The payload interface at each port has been standardized, allowing for hosted and separable payload interchangeability, late payload integration and manifest changes. 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. 97 24 Opportunity which will utilize an Evolved Expendable Launch Vehicle (EELV) Secondary Payload Adapter (ESPA) or ESPA Grande. This could include full development of a new launch system or modifications to an existing launch system, including launch infrastructure. a new EELV acquisition strategy in November 2011, revising it in 2013. Blue Origin was awarded $500 million of phase 1 funding for further development of New Glenn as a potential competitor in future contracts. [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. >>
EELV STANDARD INTERFACE SPECIFICATION VERSION 5.0. As of September 2019, it has two manifested classified national security flights for the USAF in 2021.[43][44][45]. [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. 1401 ULA has a big factory down in Decatur, Alabama. 0000002426 00000 n
The intent was to replace legacy vehicles, including Delta II, Atlas II, and Titan IV. NASA Mission Specific ESPA SIS 4 LSP-REQ-317.01B Launch Services Program Program Level Dispenser and CubeSat @(l(MW a 67E1efWmh8s`e3XY|t+$8f`~!Af6 Dy3 0000002358 00000 n
[47][48], The contract type for the phase 2 contracts is new for US government launches as it will be a "firm-fixed-price, indefinite-delivery" type of launch contract. 0000000776 00000 n
1. [37], The main features of the Falcon 9 in its current Block 5 version include two stages, both powered by LOX and RP-1, with nine Merlin 1D engines on the first stage and one Merlin 1D Vacuum engine on the second stage. %PDF-1.7
%
DOD's Evolved Expendable Launch Vehicle (EELV) program is the primary provider of launch vehicles for U.S. military and intelligence satellites. 0000002686 00000 n
The contractor was standardizing payload interfaces, launch pads, and infrastructure so that all configurations of each contractor's EELV family can be launched from the same pad and payloads can be interchanged between vehicles in the same class (i.e., medium, intermediate, or heavy). "=pdsy8&$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! %%EOF
The payload interface at each port has been standardized, allowing for hosted and separable payload inter-changeability, late payload integration, As an example, an Atlas V 551 has a 5.4m payload fairing, 5 SRBs, and 1 RL-10.[35]. New ICD Revisions in Development 8/22/2022: UPREVISIONS RELEASED hb``g``f`f`. 6 0 obj 4 0 obj [46] SpaceX received none of this funding to develop their designs, as both the Falcon 9 and Falcon Heavy had completed development and were already flying. 0000076318 00000 n
endstream [8] Some of the reasons why assured access to space is a priority for the United States are stated in National Presidential Directive Number 40, which reads: Access to space through U.S. space transportation capabilities is essential to: The United States, therefore, must maintain robust, responsive, and resilient U.S. space transportation capabilities to assure access to space. The EELV program would maintain current mass-to-orbit capability while increasing launch rate and decreasing costs. As of 2019, these launch vehicles were the primary methods for launching U.S. military satellites, along with the Falcon 9 developed by SpaceX. R'O* u/7svAZ6r4[ZDX$22L)966@D1{2?=ben6hy. The Atlas V family is capable of carrying payloads of 8,900 kg (19,620 lbs) to geosynchronous transfer orbit, and can lift 16,034 kg (35,343 lbs) to low-Earth orbit. hWn8>(o@N@-l5:l;C8y!e -TPAqPi"`[#=yb#\d8B${t)"1`c]+e2a^H5U`j"q!DqttMo"!e]N>f1/ktOD3G=M/&n y6[)*zN 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 . ULAs use of these tactics artificially created a need for relief from legislative restrictions on its ability to continue using RD-180relief that, with the DoDs active assistance, ULAs actively sought in the fiscal year 2016 omnibus appropriations bill. The Atlas V family uses a Russian RD-180 to power the first stage Common Core Booster. At the same time, another 14 boosters were to be procured competitively beginning in 2015, with the initial launches to be performed in 2017. One of the Air Forces long-term goals for the EELV program is to have at least two certified launch providers able to compete for the full range of national security launches. endobj By 2016 the Air Force was working to introduce competition into the Evolved Expendable Launch Vehicle (EELV) program. Evolved Expendable Launch Vehicle (EELV) standard interface specification, as well as Falcon 9 and Falcon Heavy. %%EOF The ESPAStar platform leverages the available mass margin from any EELV launch to provide an affordable path to space for payloads. endobj mimics the EELV 157.5 cm (62.01 in) Standard Interface Plane. xwTS7" %z ;HQIP&vDF)VdTG"cEb PQDEk 5Yg} PtX4X\XffGD=H.d,P&s"7C$ Attachment 6 Evaluation Criteria. 0000003719 00000 n
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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. 0000000956 00000 n
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The USAF and United States Space Force (USSF) plan to use the next generation NSSL launch vehicles until at least 2030.[31]. 6 0 obj << /Type /Page /Parent 3 0 R /Resources 6 0 R /Contents 4 0 R /MediaBox [0 0 612 792] Evolved Expendable Launch Vehicle (EELV) standard interface specification. 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. 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. ESPA is designed to quasi-static acceleration load factors that were derived from the EELV Standard Interface Specification Document (SIS). %PDF-1.6
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stream The launch occurred on December 23, 2018.[40].
for GPS III Launch Services . %%EOF
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Table 2 - Quasi-Static Load Factors - "Paper Session II-C - The Evolved Expendable Launch Vehicle (EELV) Standard Interface Specification For Space Vehicle Accommodations" Skip to search form Skip to main content Skip to account menu. [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. In paying ULA for such fixed launch costs and executing the EELV program under a cost-plus contract, the DoD has reimbursed ULA for allowable, reasonable, and allocable costs for its launches, while requiring ULA to reimburse it on a per-launch basis for launches that ULA sells to its non-DoD customers. 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). RFP F04701-97-R-0008 19 June 1998 ii 0000006582 00000 n
[35], A three-digit (XYZ) naming convention is used for the Atlas V configuration identification. 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). DHh0D@z5+?w
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. 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 . 0000087266 00000 n
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The US Space Force (USSF) plans 3034 launches during these five fiscal years. 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). 0000009026 00000 n
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SpaceX bid the existing launch vehicles of Falcon 9 and Falcon Heavy, while Blue Origin was expected to bid New Glenn, ULA bid Vulcan Centaur, and NGIS's bid status was not reported. [12] Boeing was awarded a contract for 19 out of the 28 launches; Lockheed Martin was awarded a contract for the other 9.
. APL requirements are not addressed in the SIS but their The payload interface at each port has been standardized, allowing for hosted and separable payload inter-changeability, late payload integration, Vehicles are defined by the number of solids and the width of the payload fairing. @(l(MW a 67E1efWmh8s`e3XY|t+$8f`~!Af6 Dy3 K0iABZyCAP8C@&*CP=#t] 4}a
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&x*sb|! Reducing the cost of launches and ensuring national access to space were the two main goals of the USAF space launch/EELV program. DOD expects to spend about $9.5 billion over the next 5 years acquiring launch hardware and services through the program, during which time it will also be working to certify new launch providers. [ /ICCBased 18 0 R ] 21 0 obj 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. 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. A Standard Payload Interface bus was also proposed as a way to save money and improve efficiency. /TT4 11 0 R >> >> 18 0 obj EELV STANDARD INTERFACE SPECIFICATION VERSION 5.0. 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