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INTEGRATED SPACE PLAN (Preliminary)

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INTEGRATED SPACE PLAN (Preliminary) CRITICAL PATH AMERICAN SPACE SHUTTLE PROGRAM INTEGRATED SPACE PLAN Space Transportation (NSTS) Systems Division FIRST INTERNATIONAL RMS GENERATION EXPENDABLE LAUNCH (INTERNATIONAL) OF VEHICLE FLEET (Preliminary) IUS UNITED STATES LAUNCH VEHICLE CAPABILITES REUSABLE SPACECRAFT PRIVATE LAUNCH VERSION 1.1 FEBRUARY, 1989 VEHICLE # TO LEO # TO GEO GEO-CIRCULAR FIRST FLIGHT VEHICLES ALS 200,000 1998 * THE AMERICAN SPACE SHUTTLE (ELV’S) EMU SHUTTLE C 150,000 20,000 (CENTAUR) 1994 1983 PRODUCED BY RONALD M. JONES D/385-210 SPACE 55,000 5,500 (IUS) 1981 1983 * CHALLENGER OV-099 SHUTTLE 6,500 (TOS) * COLUMBIA OV-102 ABOUT THIS DIAGRAM: TITAN 4 40,000 12,500 10,000 (CENTAUR) 1989 OV-103 * DISCOVERY GOVERNMENT - The Rockwell Integrated Space Plan (ISP) is a very long range systematic perspective of America’s and the TITAN 3 33,000 8,600 4,200 (IUS) 1965 MMU * ATLANTIS OV-104 COMMERCIAL SATELLITE Western World’s space program. Its 100-plus-year vision was created from the integration of numerous NASA ATLAS 2 14,400 5,200 2,500 1991 EARTH-TO-ORBIT * TBD OV-105 DEPLOYMENT long-range studies including the project Pathfinder case studies, recommendations from the National ATLAS 1 12,300 1959 AND IN-SPACE Commission on Space’s report to the President, the Ride report to the NASA Administrator, and the new DELTA 2 11,100 3,190 1,350 (PAM-D) 1988 SATELLITE RETRIEVAL * THE SOVIET SPACE SHUTTLE TRANSPORTATION SYSTEMS National Space Policy Directive. Special initiatives such as the four Pathfinder scenarios or those described in DELTA 7,800 1960 AND SERVICING * BURAN the Ride Report (i.e., Mission To Planet Earth, Exploration of the Solar System, Outpost on the Moon, and TITAN 2 5,500 1965 DEFENSE SATELLITES Humans to Mars) are integral parts of the ISP. These initiatives as well as the agenda described in the National SCOUT 475 1961 VOYAGER II SOLAR MAX / ARIANE 3 Commision on Space report, are shown by shading the appropriate boxes involved. These shaded versions are URANUS ENCOUNTER SPACE SHUTTLE ENHANCEMENTS, SPACE TELESCOPE included separately as attachments to the ISP. The ISP is not meant to be a definitive plan for the development LAUNCH VEHICLES OF EUROPE AND JAPAN PLANETARY / SCIENTIFIC MISSION TYPES of space, but rather a compilation of evolutionary opportunities for our near-term and long-range space MISSIONS INTERNATIONAL COMPETITION, YLOADS VEHICLE # TO LEO # TO GEO COUNTRY FIRST FLIGHT activities. PRECURSOR A ARIANE 4 ARIANE 3 5,690 EUROPE 1984 AN INVIGORATED ELV FLEET The ISP can be read from top to bottom or left to right. From top to bottom, vertical column elements are ARIANE 4 9,260 EUROPE 1988 ROBOTIC SPACELAB SATELLITE REFUELING TITAN 2 phased in chronologically to support centerline milestones. Reading across the columns from left to right will ARIANE 5 46,000 14,960 EUROPE 1996 EXPLORATION AND U.S. NATIONAL POLICY (INTERNATIONAL) CAPABILITY yield the total scope of required activity within a given time period in support of the total “integrated” plan. The centerline of the ISP is the critical path defined by National Space Policy which closely resembles the H-1 2,300 JAPAN 1986 SPUR SPACE RECOVERY MID-SIZE P NSTS H-2 9,000 JAPAN 1992 GPS TDRS RETURN-TO-FLIGHT NASA Office of Exploration case study 4 scenario — Lunar Outpost To Early Mars Evolution. The Space 1988 1988 CONSTELLATION CONSTELLATION Shuttle and Space Station are essential initial elements; their value increases through the 1990’s as SUBORBITAL LOFT-1 / E’PRIME infrastructure evolves. Arrowed lines between boxes depict evolutionary, supporting, or synergistic SOVIET PHOBOS ABUNDANT NEAR-EARTH EXTRATERRESTRIAL RESOURCES PAYLOAD MARKET relationships. Double-arrowed lines between boxes are communication / data links. Bold lines are trunk lines ENCOUNTER OV-105 PHOBOS/ ELEMENT EXTENDED DELTA 2 (MLV-1) with numerous (2 or more) branches stemming from along their length. Boxes with bold outlines are either RESOURCE MOON ASTEROIDS* COMETS CONTRACT AWARD DEIMOS NAME DURATION ORBITER long-range (centerline) objectives or key “enabling programs” important because their development affects the Al X ALUMINUM MAGELLAN HUBBLE TITAN 3 / 34D development of many other programs. Boxes with double lines are in-space transportation nodes. The ISP is SPACE TELESCOPE C X C X CARBON chronologically portrayed in five year time intervals because this is a practical segment of time for planning Ca X CALCIUM AND COMMERCIAL SPACE FACILITIES TITAN 4 VOYAGER II IN-SPACE and implementation of program objectives. Obviously, the dates shown have an uncertainty which increases Fe X M IRON SPACEHAB NEPTUNE with time, but the chronology is intended to be consistent. Finally, the large bubbles represent the synergistic H X C X HYDROGEN ARE WESTERN PRECURSORS RESEARCH & STARFIRE / SSI summation of the individual elements of that period. They are the highest level groups of goals: plateaus of He3 X HELIUM 3 SUBORBITAL ET DEVELOPMENT TO human achievement attainable through a comprehensive execution of the depicted ISP elements. Mg X MAGNESIUM GALILEO APPLICATIONS ILV-1 / AMROC N X C X NITROGEN GRO PERMANENT PV-105 Ni X M NICKEL EDO YLOADS PEGASUS / OSC ULYSSES DELIVERY A O X C X OXYGEN MID-SIZE PAYLOAD P ROCKWELL INTERNATIONAL Si X SILICON (INTERNATIONAL) HUMAN PRESENCE MARKET CDSF ATLAS 2 (MLV-2) Space Transportation Systems Division Ti TITANIUM 12214 Lakewood Blvd. H2O ? X C X WATER MARS IN SPACE SMALL OV-106 TETHERED JAPANESE H-2 HLC Downey, California 90241 OBSERVER * METALLIC=M EVOLVABLE OMV CONTRACT AWARD ? SYSTEMS / TSS 1993 CARBONACEOUS=C * THE SOVIET SPACE STATION FREEDOM 1993 ADVANCED SECOND Attn: Ed Repic, Project Manager 1993 SOURCE SRB / LRB Lunar and Planetary Systems LEO ET RESOURCE BASE SOLAR SAIL ELV DEPLOYMENT Mail Code AD21 LEGEND DEMONSTRATION POSSIBLITY * THE SOVIET SPACE STATION MIR ET / ACC MISSION TO PLANET LIGHTSAT CLASS ELEMENT EARTH - ELEMENT PAYLOAD MARKET ISP Program Element RESOURCE LBS/TANK NASA’S SHUTTLE “C” / NAME EVOLVABLE OTV & DATA INTEGRATION CRAF SHUTTLE DERIVED Key Enabling Program Al 56,490 HEO AND (not on the critical path) C 2,760 CISLUNAR COORBITING LOW HEAVY LIFT CAPABILITY POLAR ORBIT Cr 188 CHROMIUM TIONS FTS INCLINATION PLATFORMS In-space Transportation Node STARPROBE TRANSPORTATION MATURING TIONS ACTIITIES Cu 3,450 COPPER SOLAR ARRAYS AMERICAN NASP / X-30 Fe 415 CENTAUR / SDV AND SHUTTLE AND CREW RETURN VEHICLE US / STATION STRUCTURE (FIRST FLIGHT LATE ‘94) Plateaus or eras of human H 466 DEEP SPACE CAPABILITY APPLICA AXAF POLAR ORBITING MPE and technical achievement INTERNATIONAL ABILITY LUNAR OBSERVER OPERATIONS APPLICA Mg 268 ELV FLEET INTERNATIONAL SPACE SLC-6 VANDENBERG ENVIRONMENTAL WASTE DUMP SPACE STATION STATION MODULES Supporting, evolutionary or N 246 2 STAGE LEO-GEO-LEO SIRTF UTILIZATION CAP OBSERVATION ACC PROJECT synergistic interrelationship Ni 200 STV CAPABILITY / PLATFORMS (4 PROPULSION SYSTEMS SPUR FREE ACEHAB LOGISTICS ELEMENTS LIFT ET PLATFORMS DEPLOYED O 1,725 SP MOMV EUROPEAN ARIANE 5 AND LUNAR LANDING MISSION FOR CIT Communication or data links Si 690 ENTERPRISE LAUNCH CAPABILITY VY 1994 THRU 1997) SITE RECON ACE SHUTTLE EVOLUTIONS Ti 220 INTERPLANETARY GEO MPE BIOSPHERE PLANET EARTH DOD SPACE STATION SP HEA Trunk line (two or more branches) MISSION ? OBSERVATION ELEMENT / ACTIVITIES PLANT AND ANIMAL Zn 173 ZINC EXPANSION SPACE HARBORING / VIVARIUM LAB DOD’S ALS- MANNED POLAR PLATFORMS DEPLOYED- SERVICING / TENDING & NASA / DOD ORBITING SPACE Critical Path / Timeline LUNAR ROVER / 5 DEPLOYED 1996 - 2000 1998 FREE FLYING RESEARCH/ 1998 SPACE STATION LEO PROPELLANT DEPOT MANUFACTURING LABS HEAVY LIFT VEHICLE SHUTTLE 1998 SAMPLE RETURN PARTIALLY CLOSED SOVIET AND CHINESE COMPONENT CELSS MISSIONS ? REMOTE TENDED GEO LAUNCH VEHICLES INDEPENDENT LEO ENABLES THE EUROPEAN TRANSPORTATION NODE VARIABLE “G” BIO-MEDICAL SOLAR DYNAMICS HERMES VEHICLE # TO LEO # TO GEO MARS ACEHAB CENTAUR HLV OR MLV AND FUEL DEPOT ? IN-SPACE DEEP SPACE PLANETARY ORBITAL PLANE WESTERN ROVER / SAMPLE SP RESEARCH FACILITY DEEP SPACE MISSIONS MISSIONS DEPLOYMENT ENERGIA 220,000 RETURN MISSIONS SHUTTLE 66,000 COMMERCIAL MMW FISSION SPACE SHUTTLE PROLIFERATION OF MANNED OTV LEO QUARANTINE POWER GENERATION SL-13 43,000 (PROTON) EXTERNAL TANK PASSENGER MODULE ? SATURN-TITAN MANNED SPACE REUSABLE SPACECRAFT SL-12 43,000 (PROTON) TRANSFER VEHICLE ACTIVITY DERIVED WORKSHOPS SL-16 33,000 CASSINI MISSION COMMERCIAL AND (WET / DRY) (INTERNATIONAL) SL-4 16,500 DEFENSE SAT LAUNCHES ET DERIVED GAMMA SDI / DOD POLAR ORBIT * THE NASA NASP * BIOSPHERE RESEARCH TION SL-3 13,900 EXTERNAL TANK RAY TELESCOPE A LAUNCH PROGRAMS EXTERNAL TANK SL-14 12,100 MAN TENDED DEPLOYMENT * THE ESA HERMES MERCURY GEO * IN-SPACE COMMERCE LEO EXTERNAL TANK DERIVED PLATFORMS SL-11 8,800 ORBITER AND FACILITIES * THE NASDA HOPE SL-6 4,600 RESOURCE BASE / GRAVITY GRADIENT ACE ST THE AMERICAN NDV STABILIZATION * THE GERMAN SANGER SL-8 3,800 * SOLAR SYSTEM EXPANSION MOMENTUM RESERVOIR SSTO OPERATIONAL INCREASED AEROBRAKE CAPABILITY * THE BRITISH HOTOL LONG MARCH 3 5,500 PHOBOS SAMPLE TETHERED SYSTEMS CAPABILITY LONG MARCH 4 8,800 RETURN MISSION STRATEGIC WESTERN SOLAR POWERED UNMANNED GEO THE JAPANESE H-II MAN TENDED GEO 2003 ELECTRIC PROPULSION RESOURCE BASE COMM AND ERT EUROPEAN SP 2003 COMM PLATFORMS ON-ORBIT HOPE HEAVY AND 2003 MARS AERONOMY PLATFORM TENDING ASTRONOMY LDF ORBITAL PLANE ORBITER IN LEO MEDIUM LIFT ELV CAPABILITY LUNAR ELECTRIC PILOTED LUNAR TRANSFER LUNAR ORBIT CAPABILITY- TIONS CARGO VEHICLE RETURN-TO-MOON STAGING / FACILITY THE AMERICAN * MLV-1 LUNAR PILOTED VEHICLE SUBSTANTIAL T COMET
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