For subparagraph 2.06 (4) (k) (i), the documents are as follows:

(a)

a statement setting out the name and address of the designer of the kind of launch vehicle;

(b) the technical specifications of the kind of launch vehicle, including the technical specifications of the following systems for launch vehicles of that kind:

(i)

the structural system;

(ii)

the propulsion system;

(iii)

the fuel system;

(iv)

the electrical system, including the power supply and power distribution systems;

(v)

the electronic systems, including the guidance system, communications system, flight control system, computer system and data management system;

(vi)

the flight safety system;

(c)

a statement setting out the name and address of the manufacturer, and country of manufacture, of the relevant launch vehicles;

(d)

a description of the manufacturer's quality assurance system and system for configuration management;

(e)

written information that shows whether the manufacturer has quality assurance certification that is accepted internationally or by a competent organisation in Australia;

(f)

written information that shows whether the launch vehicles have been manufactured in accordance with, and tested and inspected having regard to, the designer's specifications and any standards for such manufacture, testing and inspection accepted by the competent authority in the country of manufacture;

(g)

the name and address of the manufacturer of each system mentioned in paragraph (b);

(h)

a description of the development, qualification and acceptance programs (including a description of the results of the qualification and acceptance verification programs) for both the hardware and software of the systems mentioned in paragraph (b);

(i)

an outline of the verification plans for both the hardware and software of the systems mentioned in paragraph (b), including information about any qualification testing, functional testing, modelling and analyses that have been carried out in relation to those systems.