Analysis of information sources in references of the Wikipedia article "Space Launch System" in Romanian language version.
42 USC 18322. SEC. 302 SPACE LAUNCH SYSTEM AS FOLLOW-ON LAUNCH VEHICLE TO THE SPACE SHUTTLE [...] (c) MINIMUM CAPABILITY REQUIREMENTS (1) IN GENERAL — The Space Launch System developed pursuant to subsection (b) shall be designed to have, at a minimum, the following: (A) The initial capability of the core elements, without an upper stage, of lifting payloads weighing between 70 tons and 100 tons into low-Earth orbit in preparation for transit for missions beyond low Earth orbit [...] (2) FLEXIBILITY [...] (Deadline) Developmental work and testing of the core elements and the upper stage should proceed in parallel subject to appro-priations. Priority should be placed on the core elements with the goal for operational capability for the core elements not later than December 31, 2016 [...] 42 USC 18323. SEC. 303 MULTI-PURPOSE CREW VEHICLE (a) INITIATION OF DEVELOPMENT (1) IN GENERAL — The Administrator shall continue the development of a multi-purpose crew vehicle to be available as soon as practicable, and no later than for use with the Space Launch System [...] (2) GOAL FOR OPERATIONAL CAPABILITY. It shall be the goal to achieve full operational capability for the transportation vehicle developed pursuant to this subsection by not later than December 31, 2016. For purposes of meeting such goal, the Administrator may undertake a test of the transportation vehicle at the ISS before that date.
NASA and the Michoud team will shortly send the first fully assembled, 212-foot-tall core stage [...] 27.6-feet-in-diameter tanks and barrels.
NASA, on the other hand, will have to add this capability to their SLS rocket, and Mr. Rosati said NASA is tracking that debut for the Artemis 3 mission in 2023.
NASA, on the other hand, will have to add this capability to their SLS rocket, and Mr. Rosati said NASA is tracking that debut for the Artemis 3 mission in 2023.
42 USC 18322. SEC. 302 SPACE LAUNCH SYSTEM AS FOLLOW-ON LAUNCH VEHICLE TO THE SPACE SHUTTLE [...] (c) MINIMUM CAPABILITY REQUIREMENTS (1) IN GENERAL — The Space Launch System developed pursuant to subsection (b) shall be designed to have, at a minimum, the following: (A) The initial capability of the core elements, without an upper stage, of lifting payloads weighing between 70 tons and 100 tons into low-Earth orbit in preparation for transit for missions beyond low Earth orbit [...] (2) FLEXIBILITY [...] (Deadline) Developmental work and testing of the core elements and the upper stage should proceed in parallel subject to appro-priations. Priority should be placed on the core elements with the goal for operational capability for the core elements not later than December 31, 2016 [...] 42 USC 18323. SEC. 303 MULTI-PURPOSE CREW VEHICLE (a) INITIATION OF DEVELOPMENT (1) IN GENERAL — The Administrator shall continue the development of a multi-purpose crew vehicle to be available as soon as practicable, and no later than for use with the Space Launch System [...] (2) GOAL FOR OPERATIONAL CAPABILITY. It shall be the goal to achieve full operational capability for the transportation vehicle developed pursuant to this subsection by not later than December 31, 2016. For purposes of meeting such goal, the Administrator may undertake a test of the transportation vehicle at the ISS before that date.
NASA and the Michoud team will shortly send the first fully assembled, 212-foot-tall core stage [...] 27.6-feet-in-diameter tanks and barrels.