14 C.F.R. Subpart B—Criteria and Information Requirements for Obtaining a License
Title 14 - Aeronautics and Space
(a) General—(1) Launch site operator. An applicant shall identify the name and address of the applicant, and the name, address, and telephone number of any person to whom inquiries and correspondence should be directed. (2) Launch site. An applicant shall provide the name and location of the proposed launch site and include the following information: (i) A list of downrange equipment; (ii) A description of the layout of the launch site, including launch points; (iii) The types of launch vehicles to be supported at each launch point; (iv) The range of launch azimuths planned from each launch point; and (v) The scheduled operational date. (3) Foreign ownership. Identify foreign ownership of the applicant, as follows: (i) For a sole proprietorship or partnership, all foreign owners or partners; (ii) For a corporation, any foreign ownership interest of 10 percent or more; and (iii) For a joint venture, association, or other entity, any foreign entities participating in the entity. (b) Environmental. An applicant shall provide the FAA with information for the FAA to analyze the environmental impacts associated with the operation of the proposed launch site. The information provided by an applicant must be sufficient to enable the FAA to comply with the requirements of the National Environment Policy Act, 42 U.S.C. 4321 et seq. (NEPA), the Council on Environmental Quality Regulations for Implementing the Procedural Provisions of NEPA, 40 CFR parts 1500–1508, and the FAA's Procedures for Considering Environmental Impacts, FAA Order 1050.1D. An applicant shall submit environmental information concerning a proposed launch site not covered by existing environmental documentation, and other factors as determined by the FAA. (c) Launch site location. (1) Except as provided by paragraph (c)(2) of this section, an applicant shall provide the information necessary to demonstrate compliance with §§420.19–420.29. (2) An applicant who is proposing to locate a launch site at an existing launch point at a federal launch range is not required to comply with paragraph (c)(1) of this section if a launch vehicle of the same type and class as proposed for the launch point has been safely launched from the launch point. (d) Explosive site plan. (1) Except as provided by paragraph (d)(2) of this section, an applicant shall submit an explosive site plan that complies with §§420.63, 420.65, 420.67, and 420.69. (2) If an applicant plans to operate a launch site located on a federal launch range, and if the applicant is required by the federal launch range to comply with the federal launch range's explosive safety requirements, the applicant shall submit the explosive site plan submitted to the federal launch range. (e) Launch site operations. An applicant shall provide the information necessary to demonstrate compliance with the requirements of §§420.53, 420.55, 420.57, 420.59, 420.61, and 420.71. (a) The FAA will issue a license under this part when the FAA determines that: (1) The application provides the information required by §420.15; (2) The FAA has completed an analysis of the environmental impacts associated with the proposed operation of the launch site, in accordance with NEPA, 40 CFR parts 1500–1508, and FAA Order 1050.1D; (3) The launch site location meets the requirements of §§420.19, 420.21, 420.23, 420.25, 420.27, and 420.29; (4) The applicant has completed the agreements required by §420.31; (5) The application demonstrates that the applicant shall satisfy the requirements of §§420.53, 420.55, 420.57, 420.59, 420.61 and 420.71; (6) The explosive site plan meets the criteria of §§420.63, 420.65, 420.67 and 420.69; and (7) Issuing a license would not jeopardize foreign policy or national security interests of the United States. (b) The FAA advises an applicant, in writing, of any issue arising during an application review that would lead to denial. The applicant may respond in writing, submit additional information, or amend its license application. (a) To gain approval for a launch site location, an applicant shall demonstrate that for each launch point proposed for the launch site, at least one type of expendable or reusable launch vehicle can be flown from the launch point safely. For purposes of the launch site location review: (1) A safe launch must possess a risk level estimated, in accordance with the requirements of this part, not to exceed an expected average number of 0.00003 casualties (Ec) to the collective member of the public exposed to hazards from the flight (Ec ≤ 30 × 10−6). (2) Types of launch vehicles include orbital expendable launch vehicles, guided sub-orbital expendable launch vehicles, unguided sub-orbital expendable launch vehicles, and reusable launch vehicles. Orbital expendable launch vehicles are further classified by weight class, based on the weight of payload the launch vehicle can place in a 100-nm orbit, as defined in table 1. (b) If an applicant proposes to have more than one type of launch vehicle flown from a launch point, the applicant shall demonstrate that each type of expendable or reusable launch vehicle planned to be flown from the launch point can be flown from the launch point safely. (c) If an applicant proposes to have more than one weight class of orbital expendable launch vehicles flown from a launch point, the applicant shall demonstrate that the heaviest weight class planned to be flown from the launch point can be flown from the launch point safely. (a) The distance from any proposed launch point to the closest launch site boundary must be at least as great as the debris dispersion radius of the largest launch vehicle type and weight class proposed for the launch point. (b) For a launch site supporting any expendable launch vehicle, an applicant shall use the largest distance provided by table 2 for the type and weight class of any launch vehicle proposed for the launch point. (c) For a launch site supporting any reusable launch vehicle, an applicant shall determine the debris dispersion radius that represents the maximum distance from a launch point that debris travels given a worst-case launch vehicle failure in the launch area. An applicant must clearly and convincingly demonstrate the validity of its proposed debris dispersion radius. (a) Guided orbital expendable launch vehicle. For a guided orbital expendable launch vehicle, an applicant shall define a flight corridor that: (1) Encompasses an area that the applicant estimates, in accordance with the requirements of this part, to contain debris with a ballistic coefficient of ≥ 3 pounds per square foot, from any non-nominal flight of a guided orbital expendable launch vehicle from the launch point to a point 5000 nm downrange, or where the IIP leaves the surface of the Earth, whichever is shorter; (2) Includes an overflight exclusion zone where the public risk criteria of 30×10−6 would be exceeded if one person were present in the open; and (3) Uses one of the methodologies provided in appendix A or B of this part. The FAA will approve an alternate method if an applicant provides a clear and convincing demonstration that its proposed method provides an equivalent level of safety to that required by appendix A or B of this part. (b) Guided sub-orbital expendable launch vehicle. For a guided sub-orbital expendable launch vehicle, an applicant shall define a flight corridor that: (1) Encompasses an area that the applicant estimates, in accordance with the requirements of this part, to contain debris with a ballistic coefficient of ≥ 3 pounds per square foot, from any non-nominal flight of a guided sub-orbital expendable launch vehicle from the launch point to impact with the earth's surface; (2) Includes an impact dispersion area for the launch vehicle's last stage; (3) Includes an overflight exclusion zone where the public risk criteria of 30×10−6 would be exceeded if one person were present in the open; and (4) Uses one of the methodologies provided in appendices A or B to this part. The FAA will approve an alternate method if an applicant provides a clear and convincing demonstration that its proposed method provides an equivalent level of safety to that required by appendix A or B of this part. (c) Unguided sub-orbital expendable launch vehicle. (1) For an unguided sub-orbital expendable launch vehicle, an applicant shall define the following using the methodology provided by appendix D of this part: (i) Impact dispersion areas that the applicant estimates, in accordance with the requirements of this part, to contain the impact of launch vehicle stages from nominal flight of an unguided sub-orbital expendable launch vehicle from the launch point to impact with the earth's surface; and (ii) An overflight exclusion zone where the public risk criteria of 30×10−6 would be exceeded if one person were present in the open. (2) The FAA will approve an alternate method if an applicant provides a clear and convincing demonstration that its proposed method provides an equivalent level of safety to that required by appendix D of this part. (3) An applicant shall base its analysis on an unguided suborbital launch vehicle whose final launch vehicle stage apogee represents the intended use of the launch point. (d) Reusable launch vehicle. For a reusable launch vehicle, an applicant shall define a flight corridor that contains the hazardous debris from nominal and non-nominal flight of a reusable launch vehicle. The applicant must provide a clear and convincing demonstration of the validity of its flight corridor. (a) If a flight corridor or impact dispersion area defined by section 420.23 contains a populated area, the applicant shall estimate the casualty expectation associated with the flight corridor or impact dispersion area. An applicant shall use the methodology provided in appendix C to this part for guided orbital or suborbital expendable launch vehicles and appendix D for unguided suborbital launch vehicles. The FAA will approve an alternate method if an applicant provides a clear and convincing demonstration that its proposed method provides an equivalent level of safety to that required by appendix C or D of this part. For a reusable launch vehicle, an applicant must provide a clear and convincing demonstration of the validity of its risk analysis. (b) If the estimated expected casualty exceeds 30×10−6, the FAA will not approve the location of the proposed launch point. An applicant shall provide the following launch site location review information in its application: (a) A map or maps showing the location of each launch point proposed, and the flight azimuth, IIP, flight corridor, and each impact range and impact dispersion area for each launch point; (b) Each launch vehicle type and any launch vehicle class proposed for each launch point; (c) Trajectory data; (d) Wind data, including each month and any percent wind data used in the analysis; (e) Any launch vehicle apogee used in the analysis; (f) Each populated area located within a flight corridor or impact dispersion area; (g) The estimated casualty expectancy calculated for each populated area within a flight corridor or impact dispersion area; (h) The effective casualty areas used in the analysis; (i) The estimated casualty expectancy for each flight corridor or set of impact dispersion areas; and (j) If populated areas are located within an overflight exclusion zone, a demonstration that there are times when the public is not present or that the applicant has an agreement in place to evacuate the public from the overflight exclusion zone during a launch. An applicant for a license to operate a launch site for an unproven launch vehicle shall provide a clear and convincing demonstration that its proposed launch site location provides an equivalent level of safety to that required by this part. (a) Except as provided by paragraph (c) of this section, an applicant shall complete an agreement with the local U.S. Coast Guard district to establish procedures for the issuance of a Notice to Mariners prior to a launch and other such measures as the Coast Guard deems necessary to protect public health and safety. (b) Except as provided by paragraph (c) of this section, an applicant shall complete an agreement with the FAA Air Traffic Control (ATC) office having jurisdiction over the airspace through which launches will take place, to establish procedures for the issuance of a Notice to Airmen prior to a launch and for closing of air routes during the launch window and other such measures as the FAA ATC office deems necessary to protect public health and safety. (c) An applicant that plans to operate a launch site located on a federal launch range does not have to comply with section 420.31 if the applicant is using existing federal launch range agreements with the U.S. Coast Guard and the FAA ATC office having jurisdiction over the airspace through which launches will take place.
Title 14: Aeronautics and Space
PART 420—LICENSE TO OPERATE A LAUNCH SITE
Subpart B—Criteria and Information Requirements for Obtaining a License
§ 420.15 Information requirements.
§ 420.17 Bases for issuance of a license.
§ 420.19 Launch site location review—general.
Table 1 of § 420.19_Orbital Expendable Launch Vehicle Classes by Payload Weight (lbs)---------------------------------------------------------------------------------------------------------------- Weight class 100 nm orbit ----------------------------------------------------------------------- Small Medium Medium large Large----------------------------------------------------------------------------------------------------------------28 degrees inclination *................ [le]4400 >4400 to >11100 to >18500 [le]11100 [le]1850090 degrees inclination.................. [le]3300 >3300 to >8400 to >15000 [le]8400 [le]15000----------------------------------------------------------------------------------------------------------------* 28 degrees inclination orbit from a launch point at 28 degrees latitude.
§ 420.21 Launch site location review—launch site boundary.
Table 2 of § 420.21_Minimum Distance From Launch Point to Launch Site Boundary (feet)---------------------------------------------------------------------------------------------------------------- Orbital expendable launch vehicle class Type of suborbital launch vehicle---------------------------------------------------------------------------------------------------------------- Small Medium Medium large Large Guided Unguided---------------------------------------------------------------------------------------------------------------- 7300 9300 10600 13000 8000 1600----------------------------------------------------------------------------------------------------------------
§ 420.23 Launch site location review—flight corridor.
§ 420.25 Launch site location review—risk analysis.
§ 420.27 Launch site location review—information requirements.
§ 420.29 Launch site location review for unproven launch vehicles.
§ 420.31 Agreements.
§§ 420.32-420.40 [Reserved]
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