ISO 17689:2015
(Main)Space systems — Interface control documents between ground systems, ground support equipment and launch vehicle with payload
Space systems — Interface control documents between ground systems, ground support equipment and launch vehicle with payload
ISO 17689:2015 is applied for organizations developing ground support equipment and also for operators performing space activity. Interface control documents format defined here does not contain the descriptions regarding various properties of ground support equipment (i.e. performance, functions or endurance to launch mechanical environment or quality assurance provisions) which are defined in technical specifications. Control of interfaces, independently of its frequency or depth, cannot replace stages of parameters definition of high-quality production and development of technical requirements of project, design and development. Interfaces control is used as a control process that can provide necessary verification of successful finishing of design at a stated in contract period. This International Standard establishes basic requirements for interface control documents (ICD) writing and interface control procedures for the following items included in launch system: payload, launch vehicle, ground support equipment (according to ISO 14625:2007) and launch site (buildings with technical systems). Notably a) ICD between payload and launch vehicle (according to ISO 15863:2003), b) ICD between ground support equipment and payload (this International Standard), c) ICD between ground support equipment and launch vehicle (this International Standard), d) ICD between items of ground support equipment (this International Standard), and e) ICD between ground support equipment and launch site (this International Standard).
Systèmes spatiaux — Documents de contrôle d'interface entre les systèmes au sol, l'équipement de soutien au sol et le véhicule de lancement de charge utile
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Standards Content (Sample)
INTERNATIONAL ISO
STANDARD 17689
First edition
2015-10-15
Space systems — Interface control
documents between ground systems,
ground support equipment and launch
vehicle with payload
Systèmes spatiaux — Documents de contrôle d’interface entre les
systèmes au sol, l’équipement de soutien au sol et le véhicule de
lancement de charge utile
Reference number
ISO 17689:2015(E)
©
ISO 2015
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ISO 17689:2015(E)
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ISO 17689:2015(E)
Contents Page
Foreword .iv
Introduction .v
1 Scope . 1
2 Terms and definitions . 1
3 General . 3
4 Requirements to ICD execution . 7
4.1 Requirements to item ICD execution . 7
4.2 Requirements to execution of summary list of launch site ICD .14
5 ICD development, validation and verification stages .14
5.1 Working stages .14
5.2 Verification and validation procedures .16
Bibliography .17
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ISO 17689:2015(E)
Foreword
ISO (the International Organization for Standardization) is a worldwide federation of national standards
bodies (ISO member bodies). The work of preparing International Standards is normally carried out
through ISO technical committees. Each member body interested in a subject for which a technical
committee has been established has the right to be represented on that committee. International
organizations, governmental and non-governmental, in liaison with ISO, also take part in the work.
ISO collaborates closely with the International Electrotechnical Commission (IEC) on all matters of
electrotechnical standardization.
The procedures used to develop this document and those intended for its further maintenance are
described in the ISO/IEC Directives, Part 1. In particular the different approval criteria needed for the
different types of ISO documents should be noted. This document was drafted in accordance with the
editorial rules of the ISO/IEC Directives, Part 2 (see www.iso.org/directives).
Attention is drawn to the possibility that some of the elements of this document may be the subject of
patent rights. ISO shall not be held responsible for identifying any or all such patent rights. Details of
any patent rights identified during the development of the document will be in the Introduction and/or
on the ISO list of patent declarations received (see www.iso.org/patents).
Any trade name used in this document is information given for the convenience of users and does not
constitute an endorsement.
For an explanation on the meaning of ISO specific terms and expressions related to conformity
assessment, as well as information about ISO’s adherence to the WTO principles in the Technical
Barriers to Trade (TBT) see the following URL: Foreword - Supplementary information
The committee responsible for this document is ISO/TC 20, Aircraft and space vehicles, Subcommittee
SC 14, Space systems and operations.
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ISO 17689:2015(E)
Introduction
This International Standard is intended for application at realization of interstate, intergovernmental
or non-governmental space activity, between operators of some country and different organizations on
the basis of their space activity contracts.
Interfaced (connected) devices development by two and more designers (commands, organizations,
developers of other specializations, etс.) creates a need for coordination between them to prevent
interfaces discrepancy for unlimited possibilities of design (construction) perfection during the
creation of space technics.
This International Standard establishes basic requirements for interface control documents (ICD)
writing and interface control procedures for the following items included in launch system: payload,
launch vehicle, ground support equipment (according to ISO 14625:2007) and launch site (buildings
with technical systems). Notably
a) ICD between payload and launch vehicle (according to ISO 15863:2003),
b) ICD between ground support equipment and payload (this International Standard),
c) ICD between ground support equipment and launch vehicle (this International Standard),
d) ICD between items of ground support equipment (this International Standard), and
e) ICD between ground support equipment and launch site (this International Standard).
ICD enables systematic creation (development), operation and management of interfaces b) to e) at
all stages of life cycle of launch system. It is necessary for the purpose of guarantee of launch system
normal functioning, prevention of accident and reduces of acceptable risk at joint space projects and
services of space vehicles insertion into space.
Application of this International Standard at design and development stages will improve control and
compatibility of all interfaces [b) to e)].
Application of this International Standard at operation stage will improve launch system safety and
facilitate control of interfaces.
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INTERNATIONAL STANDARD ISO 17689:2015(E)
Space systems — Interface control documents between
ground systems, ground support equipment and launch
vehicle with payload
1 Scope
This International Standard is applied for organizations developing ground support equipment and also
for operators performing space activity.
Interface control documents format defined here does not contain the descriptions regarding various
properties of ground support equipment (i.e. performance, functions or endurance to launch mechanical
environment or quality assurance provisions) which are defined in technical specifications.
Control of interfaces, independently of its frequency or depth, cannot replace stages of parameters
definition of high-quality production and development of technical requirements of project, design and
development. Interfaces control is used as a control process that can provide necessary verification of
successful finishing of design at a stated in contract period.
This International Standard establishes basic requirements for interface control documents (ICD)
writing and interface control procedures for the following items included in launch system: payload,
launch vehicle, ground support equipment (according to ISO 14625:2007) and launch site (buildings
with technical systems). Notably
a) ICD between payload and launch vehicle (according to ISO 15863:2003),
b) ICD between ground support equipment and payload (this International Standard),
c) ICD between ground support equipment and launch vehicle (this International Standard),
d) ICD between items of ground support equipment (this International Standard), and
e) ICD between ground support equipment and launch site (this International Standard).
2 Terms and definitions
For the purposes of this document, the following terms and definitions apply.
2.1
interface control document for ground support equipment
document which describes mechanical, hydraulic, pneumatic, thermal, electric and other parameters of
interfaces between ground support equipment and launch vehicle, items of ground support equipment,
ground support equipment and launch site objects (building constructions with technical systems), and
which is used to control these parameters
2.2
ground support equipment
units and systems necessary for the prelaunch operations and operations for launch of payload and
launch vehicle (rocket fuelling systems, gas supply systems, thermostating systems, launch pad, units
for LV installation on launch pad, ground support equipment control systems, etc.)
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ISO 17689:2015(E)
2.3
launch site
site necessary for the prelaunch and launch operations of a space vehicle and for the in-flight operations
during the launch phase
[SOURCE: ISO 14620-2:2011, 3.16]
2.4
launch system
system made up of a launch vehicle, the associated launch complex, launch site, payload, ground support
equipment and associated airborne equipment (including software), control systems, navigation
system, trajectories, procedures, necessary personnel, and any other associated items
[SOURCE: ISO 14620-2:2011, 3.18]
2.5
launch range
systems, facilities and means, not part of the launch system, required to provide the necessary service
and support for carrying out a launch campaign and to ensure safety and security of persons, assets
and protection of the environment
2.6
launch complex
site assigned to or owned by a launch vehicle operator to operate a launch vehicle
[SOURCE: ISO 14620-2:2011, 3.14]
2.7
launch vehicle
any vehicle constructed for the purpose of operating in outer space, or placing one or more payloads in
outer space, as well as any suborbital rocket
[SOURCE: ISO 14620-2:2011, 3.19]
2.8
payload
space vehicle or group of space vehicles on a single-launch vehicle intended to perform a specified
function or series of functions
[SOURCE: ISO 14620-2:2011, 3.24]
2.9
ground safety
arrangements intended to reduce and control safety risks identified in ground prelaunch and launch
activities of a manned or unmanned space vehicle
Note 1 to entry: Arrangements include protecting people, public and private property, and the environment
and completing and adjusting the national regulatory laws related to occupational safety and health, workers,
environment, space, etc.
[SOURCE: ISO 14620-2:2011, 3.8]
2.10
hazard
existing or potential condition of an item that can result in a mishap
Note 1 to entry: This condition can be associated with the design, fabrication, operation, or environment of the
item, and has the potential for mishaps.
[SOURCE: ISO 14620-2:2011, 3.9]
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ISO 17689:2015(E)
2.11
mishap
accident
unplanned event or series of events resulting in damage or potential for damage
Note 1 to entry: While sometimes used synonymously, an “accident” generally means a severe type of “mishap”.
[SOURCE: ISO 14620-2:2011, 3.20]
2.12
acceptable risk
safety risk, the severity and the probability of which may be reasonably accepted by humanity, without
durable or irreversible foreseeable consequence on health, Earth, and the environment, at the present
time and in the future
EXAMPLE A safety risk may be acceptable for crew members of a manned space vehicle when it is
comparable to that of test pilots, for the personnel participating in hazardous activities when it is comparable to
that of industrial workers, for people, public and private property, and the environment, when it is comparable to
that of other hazardous human activities (e.g. high-speed surface travel).
[SOURCE: ISO 14620-2:2011, 3.1]
2.13
interfaces controller
specialist in the scope of launch complexes or organization of space activity which controls ICD
observance by organization-executor at realization of contract of space technics creation
Note 1 to entry: Interface controller may be indicated in contract between space technics leading developer and
executors. Leading developer can let a contract with controller.
3 General
3.1 ICD for ground support equipment is developed as separate document for each part included
in launch system: payload, launch vehicle, items of ground support equipment, launch site (building
constructions with technical systems):
a) ICD between ground support equipment and payload (this International Standard);
b) ICD between ground support equipment and launch vehicle (this International Standard);
c) ICD between items of ground support equipment (this International Standard);
d) ICD between ground support equipment and launch site (this International Standard).
The leading enterprise-developer of ground support equipment is responsible for the development of a
list of ICD for this equipment.
The leading enterprise-developer of a launch site supervises types, quantity and location of interfaces
of ground support equipment items which were developed by the enterprises according to ICD for items.
The developers of items of a launch site develop ICD and coordinate them with other enterprises which
are developers of the items which are interfaced.
3.2 The initiative in determination of interfaces design belongs to the enterprise having a ready
(existing) item or element of the device in relation to the enterprises which should develop an interfaced
item or device at participation in the joint project.
The organization which performs launch services of space vehicles gives the full information about
interfaces of launch pad to the organization which orders the launch services.
The payload authorities shall provide interface condition to operator.
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ISO 17689:2015(E)
3.3 It is necessary to have a note in the technical specification about presence of ICD on item.
Each interface shall have the code which contains the basic information about it.
EXAMPLE ICD XXXX-YYYY-000-ААА – interface code, where
— XXXX is the source item code,
— YYYY is the consumer item code,
— 000 is the interface number, and
— ААА is the code of place where the interface is located.
After interface number, a reference number or code (in brackets) may indicate the drawing (list) where
this interface is figured.
EXAMPLE А110-B010-001-005 (А110.08.03.01).
Number of symbols and use of figures and letters in index should correspond to approved codes in
technical specifications.
3.4 ICD can be drawn in the form of text, in the form of picture (drawing) or in complex (text and
picture) form.
The specific indicator like the letter «G» may be added separately t
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