RECOMMENDATIONS OF THE PRESIDENTIAL COMMISSION The Commission has conducted an extensive investigation of the Challenger accident to determine the probable cause and necessary corrective actions. Based on the findings and determinations of its investigation, the Commission has unanimously adopted recommendations to help assure the return to safe flight. The Commission urges that the Administrator of NASA submit, one year from now, a report to the President on the progress that NASA has made in effecting the Commission's recommendations set forth below: I DESIGN The faulty Solid Rocket Motor joint and seal must be changed. This could be a new design eliminating the joint or a redesign of the current joint and seal. No design options should be prematurely precluded because of schedule, cost or reliance on existing hardware. All Solid Rocket Motor joints should satisfy the following requirements: The joints should be fully understood, tested and verified. The integrity of the structure and of the seals of all joints should be not less than that of the case walls throughout the design envelope. The integrity of the joints should be insensitive to: --Dimensional tolerances. --Transportation and handling. --Assembly procedures. --Inspection and test procedures. --Environmental effects. --Internal case operating pressure. --Recovery and reuse effects. --Flight and water impact loads. The certification of the new design should include: --Tests which duplicate the actual launch configuration as closely as possible. --Tests over the full range of operating conditions, including temperature. Full consideration should be given to conducting static firings of the exact flight configuration in a vertical attitude. INDEPENDENT OVERSIGHT The Administrator of NASA should request the National Research Council to form an independent Solid Rocket Motor design oversight committee to implement the Commission's design recommendations and oversee the design effort. This committee should: Review and evaluate certification requirements. Provide technical oversight of the design, test program and certification. Report to the Administrator of NASA on the adequacy of the design and make appropriate recommendations. II SHUTTLE MANAGEMENT STRUCTURE The Shuttle Program Structure should be reviewed. The project managers for the various elements of the Shuttle program felt more accountable to their center management than to the Shuttle program organization. Shuttle element funding, work package definition, and vital program information frequently bypass the National STS (Shuttle) Program Manager. A redefinition of the Program Manager's responsibility is essential. This redefinition should give the Program Manager the requisite authority for all ongoing STS operations. Program funding and all Shuttle Program work at the centers should be placed clearly under the Program Manager's authority. ASTRONAUTS IN MANAGEMENT The Commission observes that there appears to be a departure from the philosophy of the 1960s and 1970s relating to the use of astronauts in management positions. These individuals brought to their positions flight experience and a keen appreciation of operations and flight safety. NASA should encourage the transition of qualified astronauts into agency management positions. The function of the Flight Crew Operations director should be elevated in the NASA organization structure. SHUTTLE SAFETY PANEL NASA should establish an STS Safety Advisory Panel reporting to the STS Program Manager. The Charter of this panel should include Shuttle operational issues, launch commit criteria, flight rules, flight readiness and risk management. The panel should include representation from the safety organization, mission operations, and the astronaut office. III CRITICALITY REVIEW AND HAZARD ANALYSIS NASA and the primary Shuttle contractors should review all Criticality 1, 1R, 2, and 2R items and hazard analyses. This review should identify those items that must be improved prior to flight to ensure mission safety. An Audit Panel, appointed by the National Research Council, should verify the adequacy of the effort and report directly to the Administrator of NASA. IV SAFETY ORGANIZATION NASA should establish an Office of Safety, Reliability and Quality Assurance to be headed by an Associate administrator, reporting directly to the NASA Administrator. It would have direct authority for safety, reliability, and quality assurance throughout the agency. The office should be assigned the work force to ensure adequate oversight of its functions and should be independent of other NASA functional and program responsibilities. The responsibilities of this office should include: The safety, reliability and quality assurance functions as they relate to all NASA activities and programs. Direction of reporting and documentation of problems, problem resolution and trends associated with flight safety. V IMPROVED COMMUNICATIONS The Commission found that Marshall Space Flight Center project managers, because of a tendency at Marshall to management isolation, failed to provide full and timely information bearing on the safety of flight 51-L to other vital elements of Shuttle program management. NASA should take energetic steps to eliminate this tendency at Marshall Space Flight Center, whether by changes of personnel, organization, indoctrination or all three. A policy should be developed which governs the imposition and removal of Shuttle launch constraints. Flight Readiness Reviews and Mission Management Team meetings should be recorded. The flight crew commander, or a designated representative, should attend the Flight Readiness Review, participate in acceptance of the vehicle for flight, and certify that the crew is properly prepared for flight. VI LANDING SAFETY NASA must take actions to improve landing safety. The tire, brake and nosewheel steering systems must be improved. These systems do not have sufficient safety margin, particularly at abort landing sites. The specific conditions under which planned landings at Kennedy would be acceptable should be determined. Criteria must be established for tires, brakes and nosewheel steering. Until the systems meet those criteria in high fidelity testing that is verified at Edwards, landing at Kennedy should not be planned. Committing to a specific landing site requires that landing area weather be forecast more than an hour in advance. During unpredictable weather periods at Kennedy, program officials should plan on Edwards landings. Increased landings at Edwards may necessitate a dual ferry capability. VII LAUNCH ABORT AND CREW ESCAPE The Shuttle program management considered first-stage abort options and crew escape options several times during the history of the program, but because of limited utility, technical infeasibility, or program cost and schedule, no systems were implemented. The Commission recommends that NASA: Make all efforts to provide a crew escape system for use during controlled gliding flight. Make every effort to increase the range of flight conditions under which an emergency runway landing can be successfully conducted in the event that two or three main engines fail early in ascent. VIII FLIGHT RATE The nation's reliance on the Shuttle as its principal space launch capability created a relentless pressure on NASA to increase the flight rate. Such reliance on a single launch capability should be avoided in the future. NASA must establish a flight rate that is consistent with its resources. A firm payload assignment policy should be established. The policy should include rigorous controls on cargo manifest changes to limit the pressures such changes exert on schedules and crew training. IX MAINTENANCE SAFEGUARDS Installation, test, and maintenance procedures must be especially rigorous for Space Shuttle items designated Criticality 1. NASA should establish a system of analyzing and reporting performance trends of such items. Maintenance procedures for such items should be specified in the Critical Items List, especially for those such as the liquid-fueled main engines, which require unstinting maintenance and overhaul. With regard to the Orbiters, NASA should: Develop and execute a comprehensive maintenance inspection plan. Perform periodic structural inspections when scheduled and not permit them to be waived. Restore and support the maintenance and spare parts programs, and stop the practice of removing parts from one Orbiter to supply another. CONCLUDING THOUGHT The Commission urges that NASA continue to receive the support of the Administration and the nation. The agency constitutes a national resource that plays a critical role in space exploration and development. It also provides a symbol of national pride and technological leadership. The Commission applauds NASA's spectacular achievements of the past and anticipates impressive achievements to come. The findings and recommendations presented in this report are intended to contribute to the future NASA successes that the nation both expects and requires as the 21st century approaches.